CA1239749A

CA1239749A - Fiber-reinforced syntactic foam composites and method for forming same

Info

Publication number: CA1239749A
Application number: CA000480831A
Authority: CA
Inventors: Janet E. Freeman; Pont Preston S.. Du; Robert E. Ritter; Alois Wittmann
Original assignee: Hughes Aircraft Co
Current assignee: Raytheon Co
Priority date: 1984-05-07
Filing date: 1985-05-06
Publication date: 1988-07-26
Also published as: US4595623A; JPS61501211A

Abstract

ABSTRACT
Fiber-reinforced syntactic foam composites having a low specific gravity and a low coefficient of thermal expansion suitable for forming lightweight structures for spacecraft applications are prepared from a mixture of a heat curable thermosetting resin, hollow microspheres having a diameter of about 5 to 200 micrometers and fibers having a length less than or equal to 250 micrometers.

Description

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FIBER REINFORCED SYNTACTIC' FOAM COMPOSITES
END METHOD OF FORMING SOME

1. yield of the Invention The present invention relates, in general, to syntactic foam composites and, more particularly, to fiber-reinforced thermosetting resin based syntactic foam composites exhibiting a low specific gravity and a low coefficient of thermal expansion.

2. Description of the Prior Art A continuing objective in the development of satellites it to optimize satellite payload weight.
One means of achieving this objective is to reduce the intrinsic weight of various operational elements within I the spacecraft. It has been recognized by the art that the desired weight reduction could be realized by replacing conventional materials, such as Lyman, with lower density synthetic composites possessing requisite mechanical thermal and chemical stability.
Included in these low density synthetic composites is a group of materials referred to in the art a syntactic foam.

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,, 1 syntactic foams are produced by dispersing microscopic rigid, hollow or idea particle in a liquid or ~emi-liquid thermosetting resin and then hardening the 5y5tem by curing The particle are generally spheres or micro balloons of carbon, polystyrene, finlike ruin ur~a-formaldehyde resin glass, or silica, ranging from 20 to 200 micrometer in dotter Commercial micro spheres have specific gravities raying from 0.033 Jo 0.33 for hollow spheres and up to 2.3 for solid glass spheres. The liquid resins used are the usual resins used in molding reinforced articles, ego, epoxy resin, polyesters, and urea-formaldehyde resins In order to form such foams, the resin containing a curing agent therefore and micro spheres may be mixed to form pate which is then cast into the desired shape end cured to form the foam. The latter method, as well as other known methods for forming syntactic foams, it described by Patrimony et at in the publication entitled Syntactic Foams I. Preparation Structure, and Proprieties in the Journal of Cell _ r Plastic, July/Augu~t 1~80, pages 223-229. When abreacted in large block form, such foams possess a compressive trench which ha jade them suitable for use in submerged tractor. In addition, the more pliable versions of the foam are utilized as filler materials which, after hardening, function as machinable, local-densification substance in applications such as automobile repair and the f tiling of structural honeycombs. Despite these characteristics of adequate compressive strength, good machinability, and light weight such foams lack the degree of dimensional and thermal stability required to render them applicable for the spacecraft environment More ~peci~ically, syntactic foam systems tend to exhibit varying filler orientation and distributions within the geometrical areas in a molded intricate structure, which limits the structural intricacy that

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1 can be achieved, as jell as reducing dimensional stability If syntactic foam systems are too highly Pulled sacrifices art jade in moldability, efficient of thermal expansion, strength, density, dimensional stability end stiffness. moreover, such foams tend to zebu poor adhesion to metallic plating which is required to form the desired product, such as an antenna component In order for the syntactic foam to be useful as a substitute for aluminum in antenna and antenna microwave components in a spacecraft, the foam must have the following characteristics.
I the material use have a specific gravity of 1.00 or less, us compared to a specific gravity of 2.7 for aluminum.
(2) The material must have a linear Coffey-client of thermal expansion or CUTE) comparable to that of aluminum, preferably clove to 13 x 10-6 in/in/F (23 x 10-6 cm/cm/C) or less.
Thermal distortion of antenna components subjected to thermal cycling in the extremes of the space environment is a major contributing factor to gain loss, pointing errors, and phase shifts.
(3) The material just meet the National Aeronautics and Space Administration (NASA) outguessing requirements to insure that thy material does not release gaseous component substances which undesirably accumulate on other spacecraft parts on the outer-space vacuum.
( 4 ) The material must have long-term stability us required for parts exposed to the space temperature environment (erg., -100F to 2509F or -73C Jo 121C) for extended periods of time, such as 10 years.

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1 US) The material must be capable of being cast into complex configurations in order to form component parts for antenna tractors ugh as wave guides or antenna feed distribLt~on networks.
The art, until the present invention, has been unable to satisfy these requirements and particularly the requirement for a low coefficient of eerily expansion I Thus, known epoxy resin based syntactic foams filled with 10 to 30% by volume hollow micro spheres generally have a in the range of 17 to 36 x 10-6 in/in/'F
(30 to 65 x 10-6 cm/cm/C~O
A need, unsatisfied by existing technology, has thus developed for a syntactic foam materiel which is both lightweight and of sufficient mechanical, thermal and chemical stability to enable it to be substituted for aluminum in physically demanding satellite environments.

SUMMARY OF THE INVENTION
The unresolved needs of the art are satisfied by the present invention which provides thermally twill fiber-reinforced syntactic foam composites having a specific gravity of 10ss than 1.0 and a linear coefficient of thermal expansion of about 25 x 10-6 inJin/F
(45 x 10-6 cm/cm/C) or less, which are prepared from an admixture of a heat curable thermosetting resin, hollow ionospheres having a diameter between about 5 and about 200 micrometers and fibers having a length of about 50 to about 2$0 micrometers.
The syntactic foam composites of the present invention can be cast as complex structures which contain lightweight hollow micro spheres having fibers, such us graphite fibers, in the voids between the micro spheres, with the micro spheres and fibers being I

1 bonded together by the heat cured resin matrix. The composites of the present invention readily meet the specific gravity, coefficient of thermal expansion and NASA outguessing requirement, which easily qualify the composites AS aluminum substitutes for spacecraft use . .
ENTAILED DESCRIPTION OF TOE INVENTION
In order to form the fiber~resin-microsphere composite of the present invention having the desired density and coefficient of thermal expansion each of the three components must be selected eon that the resulting combination thereof provides a mixture amenable to being cast into the desired configuration, as well as providing a final product having the required structural and physical properties. Acceptable mixtures must hove a viscosity that produces an accurate, void-free casting with uniform material properties. In addition the proportion of fiber in the composite must provide the required thermal expansion, strength, and I stiffness properties Further, the micro sphere component must be chosen to provide the required low density in the composite. Finally, each of the components must be capable of being combined with the other components and the effect of each on the other in the mixture thereof, a well a in the final composite must be taken into account In particular the properties of the composite are influenced by the properties, relative volume ratios, and interactions of the individual components.
More specifically, density, strength, stiffness (brittleness), coefficient of thermal expansion and processibility are strong functions of filler and fiber type volume ratios and micro packing. The following discussion provides a more detailed consideration of those various factor. It should be noted that in the l following discussion, the term syntactic foam it used herein to denote a filled polymer made by dispersing rigid, microscopic particles in a fluid polymer or resin and then curing the resin as is known in the S art. The term fiber reinforced syntactic foam composite is used rein to denote the cured product wormed from the mixture of resin micro balloons, and reinforcing fibers in accordance with the prevent invention.

l. teat Curable Resin he heat curable, thermosetting resins used to prepare the syntactic foam composites of the present invention can be any heat curable thermosetting resin having appropriate viscosity for casting (en., less than 1000 centipoise), pot life (ecg.t greater than 2 hours), coefficient of thermal expansion, and thermal stability in the temperature range of -100F to 250F
(-73C to 121C) required in the space environment.
The resin material contains a curing agent which reacts with the resin to produce a hardened material. Curing agent and other additives will, of course affect the viscosity and other properties of the final mixture from which the composite it formed Examples of suitable resins include low viscosity, polymerizable liquid polyester resins which comprise the product so the reaction of at least one polymerizable ethylenically unsaturated polycarboxylic acid, such us malefic acid or its android, and a polyhydric alcohol, such as, for example, propylene glycol and optionally, vine or more I saturated polycarboxylic acids, such as for example, phthalic acid or its android. Other suitable resin include condensates of formaldehyde such as urea-formaldehyde, melamine-formaldehyde and phenol-formaldehyde resins. Preferred resins for use in the practice of the prevent invention are epoxy resins having 1~2 epoxy groups or mixtures of such resins, and include cycloaliphAtic epoxy resins such as the glycidyl ethers of polyphenols, liquid Bisphenol-A
diglycidyl other epoxy resin (such as those told under the-tradeMarks upon 815, Eon 825, Eon 828 by Shell Chemical Company), phenol formaldehyde novolac polyglycidyl ether epoxy resins (such as those sold under the trademarks DEN 431, DEN 438 and DEN 439 by Dow Chemical Company), and epoxy crossly novolacs (such as those sold under the trademarks CON 1235, EON 1273, EON 1280 and CON 1299 by Cuba Products Company).
The particular epoxy rains preferred in the practice of the present invention are polyglycidyl lo aromatic amine, ire. ~-glycidyl amino compounds prepared by reacting a halohydrin such as epichlorohydrin with an amine, Examples of the most preferred polyglycidyl aromatic amine include di~lycidylaniline, diglycidyl orthotoluidine, tetraglycidyl ether of ethylene dianiline and tetraglycidyl m0~axylene Dunn, or mixtures thereof.
The epoxy resins which are preferably in liquid form at room temperature are admixed with polyfunctional curing agents to provide heat curable epoxy rosins which are cross-linkable at a moderate temperature, e.g., about 100C, to form thermoses articles. Suitable polyfunctional surging agent for epoxy resins include aliphatic polyamides of which diethylene thiamine and triethylene tetramine are exemplary; aromatic amine of which ethylene dianiline~ mote phenylene Damon, 4J4' diam~nodiphenyl 8ulfone are exemplary; and polycarboxylic acid androids of which pyromelli~ic dianhydride, ~enzophenone tetracarboxylic dianhydride, hexahydrophthalic android, nadir methyl android Milwaukee android adduce of methyl cyclop~ntadiene), 8 ~L~397~

1 methyl tetrahydrophthalic android and methyl hexahydrophthalic android are exemplary. Polycarboxylic acid android compounds are preferred curing guts for the above-noted preferred epoxy resins, it the three compounds last noted being ought preferred.
In preparing heat curable, thermosle~in~, epoxy resins compositions, the epoxy resin is mixed with the curing agent in proportions from about 0.6 to about 1.0 of the ~toichiometric proportions, which provides suffix client android groups and carboxylic acid groups to react with from bout 60 to 90 percent of the epoxide group.
The term cowering as used herein denotes the conversion of the thermosetting resin into an insoluble and infusible cross-linked product and, in particular, as a rule, lo with simultaneous molding to give shaped articles.
It addition curing accelerators may be added to the epoxy resins, as it known in the art, to provide a low curing temperature. Preferred accelerators or the above-noted preferred polyglycidyl aromatic amine resins are substituted imidazolçs, such as 2-ethyl-4-methyl imidazole, and organometalllc compounds, such as Tunis octet, cobalt octet, end dibutyl tin dilaurate which are incorporated at a concentration of zero to about 3 parts by weight per 100 parts resin.
Moreover, other materials may be added to the epoxy material in order to improve certain properties thereof, as is known in the art. For example, the tendency of the resin to separate from the mixture can be minimized by the addition of fine particulate filler, such as Cab-O-Sil (a fused silica manufactured by Cabot Corporation, acicular fibers, such as tall, or short chopped or milled fibers In addition, resin penetration of thy filler may be enhanced by the addition of a titan ate wetting, agent, such as CRUSOE an isopropyl tri(divctylpyrophosphate~ titan ate, availably from Enrich Petrochemical Co.

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1 p~r~icul~rly useful resin composition for forming the composite of the present invention comprises a polyglycidyl aromatic amine, a polycarboxylic acid android curing agent, and a curing alccelQrator7 sample 3 end 4 herein ore directed to the use of this preferred Resin onmulation in the practice of the pronto ~nventionO

The syntactic foam computes prepared in accordance with the prcs~nt invention contain relatively uniform distribution of hollow ~icro~phere~ These hollow microphones I usually hollow thermoplastic spheres composed of acrylic-type resin such us polymethyl-~ethacryl~te, acrylic modified styrenes polyvinylidenechlorlda or couplers of Turin and methyl methacrylate;
finlike resins; or hollow glad, silica or carbon spheres that are very light in weight end act as a lightweight filler in the syntactic ohm These micro sphere preferably have diameter in the rang of about 5 Jo about 200 ~icromater~. Method for the production of these hollow microspore are wow known in the art end are diBCU8~d, 40r ~xampl~, by Harry await and John VOW Milwaukee in thy book entitled, handbook of Falser and R~lnforce~ents for Pl~stics,J Chapter 19:
Hollow Spherical Fuller, Van Nostrand Reinhold 1978.
Such micro spheres are readily available commercially.
These hollow micro spheres can be compressed somewhat when subjected to external pressure.

1 however, they are relatively fragile and will collapse or fracture at high pressures Therefore, there is a pressure range under which the micro spheres con effectively operate, It has been determined that when hollow glass micro spheres are employed in the practice of the present invention, syntactic foam composites can by molded at pressures up to the limit ox the hollow ionospheres wow fracture, with molding pressures in the rang of about 700 to about 900 pi t0.102 to 0.131 Pascal) being preferred.
By controlling the amount of hollow micro spheres added to the syntactic form, it it possible to control the specific gravity of the foam A simple mixture of an epoxy material end hollow micro spheres tend to separate on standing, with the micro balloons rising to the surface of the epoxy However it has teen found that with an increased volume of micro balloons added to the epoxy, there is a decreased tendency to separate into discrete phases, moreover, it has been found I thaw at a sufficiently high loading of micro balloons, namely about 65% by volume for microballoons7 the tendency to separate into discrete phases is minimized.
To achieve specific gravities of lets than 1.0, the hollow micro spheres are included in the syntactic foam in up to 65% by volume and generally in a range of about 35 to about 65~ by volume and preferably about 50 to about 65~ by volume. The volume percentage of hollow microsphergs is adjusted based on the composition of the hollow micro sphere selected, the brand of micro-I spheres and the size of the micro spheres. There~ore,it may be necessary to select the proper mixture of heat curable resin material and hollow micro spheres for preparation of the syntactic foam on a trial and error basis. For example, the C15/250 series of lass micro spheres available from the EM Company has a specific gravity of Owls and a mean diameter of 50 micrometers.

1 ~Carbospher~ carbon ionospheres available from the Varier Corporation have a specific gravity of 0.32 end a mean diameter of So micrometers. Desirably, a inure of two or Gore types of hollow ~icro~phere~ Jay be S employed in the practice of the present invention. The glass ~i~ro~pheres provide the syntactic foam with improved structural strength, while those of carbon advantageously contribute to both a lowered coefficient of thermal expansion end greater amenability to Subsequent metal-plating operations. When using a combination of glass end carbon micro~ph~r~s in preparing the compute of the present invention, the ratio of glass micro spheres to carbon micro sphere it about 1:4 to lsl.
Furthermore, it has been found by using packing theory that an increased volume percent old in the reloan mixture con be achieved Packing theory it based on the corlcept that, nine the largest particle size filler on go particular reinforcement 8y8t~m packs to produce the Roy; volume of the system, the addition of ~ucceedingly smaller particles can be done on such a way as to finely occupy the voids between the larger filler without expanding thy total volume. This theory it discussed by Harry S. Razz and John V0 Milwaukee, in thy book title handbook of Filler and Reinforcements for Pla3tic~,a Chapter 4. Packing Concept in Utilization of pillar and Reinforcement Combinations, Van Nostrand Reinhold 1978. The fillers used in the present invention are chosen on the by of particle size, Shea and contribution to overall composite properties.
This theory ply Jo the use of solid particulate as well a hollow pharaoh Because of the high iota of such a highly loaded resin, the mixture could not flow into the mold without damaging the microspheresD

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1 To overcome this problem, the told is repacked with the dry filler it a mixture of ionospheres and fibers). By applying pocking o'er as described above, the filler con be packed at high density and Jo that segregation of ingredients does not occur.
Finally, the ionospheres may be advantageously treated with a coupling and wetting agent to enable the resin to wet the sphere surfaces end promote good filler-resin adhesion, as discussed in greater detail below with regard to similar treatment of the fibers used in the present invention.

3. Fibers The fibers used in the practice of the present lo invention must be compatible with the selected resin in order to provide good coupling between the fixer and resin. Fibers such as graphite, glass, Cavalier Jan aromatic polyamide material obtained from E. It Dupont and Company) nylon, or carbon are added to the syntactic foam composite of the present invention to improve the strength and dimensional stability of the composite.
however, the contribution of the fiber to the coefficient of thermal expansion of the composite product and to the viscosity ox the mixture of Components just also be considered. Graphite fibers have been found to be particularly useful wince they provide the desired strength in the composite, while also reducing the coefficient of expansion of the composite. An additional factor to consider fiber length. While shorter fibers ego. having a length-to-diameter ratio of less than loos) provide less reinforcement per fiber than do longer fibers, shorter fibers have less impact on the viscosity of the mixture. Thus, a greater volume fraction of shorter fibers can be incorporated into a 3 ~3~7~

1 mixture Ivan level of viscosity, which provides a higher level of reinforcement at that vacuity level by shorter fiber. In addition, the use of shorter fiber improves the uniformity of the mix. Thus, S fibers useful in the composite of the prevent invention have a length let than or equal to 250 micrometers end generally on the range of bout 50 lo about 250 micrometers. Fibers having length bout 150 to bout 2S0 micrometer were found to provide the best 13 compromi~ between viscosity end reinforcement as ducked previously when graphite fiber, the preferred fiber material it used, the diameter of the graphite giber it on the range of about 5 to bout 10 micrometers.
Moreover, the interaction of the fibers with the micrQspheres discussed previously must be considered.
It his been determined by microp~cking theory, as described in Chapter of the book by Katz and ~ilewski, previously referenced, that the optimum ratio of fiber-tougher varies with ho length/diameter ratio LO
of the pharaoh and with the ratio of thy ~phere-diameter to the fiber-diamet~r OR). For each flu of Lo there it on R value where the packing efficiency it Nero; end as R increases or decreases on either side of thy nimumO packing efficiency inquiries. It has been found most derby in the practice of the present invention to Use graphite fibers ox the micrometer length dusked above, which have a length to diameter ratio LO ox bout 5.1 to bout 30:1 and preferably about 15~1 to about 30~ no a ~phere-diameter to fiber~di~meter ratio (R3 of at least about sly and preferably bout sly Graphite fiber used in the practice of the prune invention are selected to have high length and low density Celan~e~GY 70 graphite fiber and Chortled HUMS graphite giber are especially suitable.

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1 Sullenness JOY fiber is 3 micrometers in diameter, has a tensile strength of 76~000 pounds per square inch ~3.6389 x 106 pa Jo a specific gravity of 1~83 ~m/cm3 and an of -0.3 x 10-6 in/in~F. Court,aulds HUMS
graphite fibers have a diameter of 8 micrometers, a tensile strength of 50,00Q psi ~2.394 x 106 Pa), a specific gravity of 1~91 gm/cm3 and longitudinal of -1 x 10 6 in/in/VF. The graphite fibers ore commercially available as ~ontinuous-fiber tows For example; Sullenness JOY fiber consists of 384 fibers/tow, The f giber tow are reducible to required lengths on the order of between about 50 micrometers and 250 micrometers by ball willing or from commercial processing concern such as the Courtaulds Company of the United Kingdom The amount of fiber incorporated in the resin-microsphare admixture generally ranges from bout 3 to about 10 volume percent and preferably from about 3 to about S volume percent in order to achieve composites having a values of 25 x 10-6 in/in~F (45 x 10-~ cm/cm/C) or less As the amount of hollow microphones and fibers incorporated in the heat curable resin increase, where it a corresponding increase on the viscosity of the resin. High viscosity prevents uniform dispersion of the micro spheres and fibers and interferes with the processing of the resin microsphere-fiber mixture during molding operations. However in order to reduce the viscosity of the mixture, the surfaces of the micro spheres and fibers may be provided with a thin layer of coupling I and wetting agents. The micro sphere and fiber surfaces ore treated with a solution containing a Solon coupling agent such as Solon A-186 (beta~-3,4-epoxy cyclohexyl)-ekhyltri~ethoxy Solon), Solon A-1120 beta ~aminoethyl~-gamma-a~inopropyl tri-methoxy-silane) or a ~L~3~'7~3 1 titsnate coupling agent such as di(dioc~ylpyrophos-phato)ethyl~ns titan ate 5RR238M available from Enrich Petrochemical Company of Bayonne, New Juries or twitter diallyloxymethyl-l-butoxy)titanium di(ditridecyl fifty ~RR55 available from enrich) or titanium di(~umylp-~enyla~e) oxy~ceta e (~R134S available from Enrich); or isopropyl tridodecylbenzenesulfonyl (RR9S available from Enrich). The coupling agents enable the resin to wet the sphere end fiber surfaces, and promote a stronger bond between thy resin, microsph~res, and fibers without increasing the viscosity appreciably.
Thy coupling agents Jay be applied by simply dissolving the junta in the resin-microsphere-fiber blend. Optionally, these gents may be applied by 5 first dissolving the agents at concentration of 0.1 - OOZE of the filler weight in water or an orçlanie solvent such us isopropanol or Freon Tao fluorocarbon compound Available from EYE Dupont end Companies and thin immuring the microphone and ibis which have 0 been premixed in predetermined proportion in the solution for a period of 5 to 30 inures followed by filtering and drying the mixture The microsphere-fiber mixture Jay then be blended with the heat curable resin preparer Jo fabricating the syntactic foam composite.
4. O~tional_Microb~ad~
Solid ~icrobead~ may optionally be incorporated in thy composite of the present invention in order to inquiry e packing efficiency. Advantageously, such microbes were also found to decrease thy v~co~ity of the formulation, improve its pour ability, and increase composite uniformity. In a preferred practice of the present invention, about 2 Jo about 8 percent by volume of idea inert material, such as glass or silica micro-beads hiving a diameter of about 2 to about 8 micrometers Jo and a specific gravity of 2,2 to 2~4 are incorporate din the r~sin~microsphere-fiber admixture. Volume percentages in excess of I increase the viscosity of the uncured, filled heat curable rosin formulation to a level at which it is unworkable for molding purposes In addi~i~n~ it was found that large filler volume fractions (volume of ~icroballoonst fiber end ~icrobead~
greater than 60 percent) had a reduced coefficient of thermal expansion, but the viscosity of the mix way unworkable. small volume fractions of filler it volume ox micro balloons, fiber, and micro beads less then 40 percent) were found to improve proce~sability, but increased the coefficient of thermal expansion to an unacceptable level. However, by choosing a filler combination that maximized filler volume yet minimized filler surface area, both viscosity end the coefficient of thermal expansion were reduced. Such a combination way used in the reinforced syntactic foam RSF-34F shown in Table III, which was procassable, uniform, had good physical properties, and was successfully cast in a metal mold.
In preparing syntactic foam by the method of the present invention, the hollow micros~heres and graphite fiber, an optionally toe solid micro beads, are admixed with the heat curable resin in any conventional fashion using a suitable mixing device such as a Waring blender.
The homogeneous admixture is then debased as by applying a vacuum. Then the mixture is loaded into a mold of suitable configuration from a reservoir or by using an sir gun or other conventional loading device. The shape of the mold will, of course, determine the shape of the cured product and Jay by chosen as required to form a desired Structure such as an antenna wave guide. Molding it then accomplished in an aut~elave at the temperature l at which the resin is curable, erg. to ~50 to 350~F
SKYE Jo 177~C~, or pow resins generally and about 150F to 250F ~66 to 121C) for the preferred epoxy composition described herein at 50 to 100 psi (2586 to 5171 mm I or OWE to 14.5 x 10-3 Pa) for about 2 to about 4 hours.
Molding of the filled heat curable resin formula-lions to Prom syntactic foam composites of the present inYen~ion may also be effected by other conventional I molding ye hods including transfer molding and compression molding procedures wherein the heat curable formulation it cured at the above-noted curing temperatures, using pressures on the order of 800 to 1000 psi (41372 to 51715 mm I or OWE to 0.145 Pascal) for 1 to 2 hours.
It has been found particularly advantageous to form the filled heat durable resin mixtures into the syntactic foam composites of the present invention by vacuum liquid transfer molding process In this procedure, the mold is first loaded with the micro sphere/
fiber filler which has been mechanically or manually premixed in predetermined proportions and pretreated with a sizing agent as previously described. text, the mold Jay optionally be vibrated to promote a uniform distribution of the filler in the mold ego n about 5 minutes on a vibration tubule Thin the mold cavity is filled with the heat durable resin. The mold is a sealable pressure vessel constructed to support the vacuum/pressure sequence described below. To prepare for the molding process, the mold cavity is I preheated Jo bring the cavity up to the temperature at which thy heat curable resin it curable A vacuum is when drawn on the mold to degas the mold cavity contents and to impregnate the filler with the resin.
The vacuum it released to atmospheric pressure to ~23~

1 burst any was bubbles remaining in the told contents Then, a ~uperatmospheric pressure, such as 100 to 1000 psi (0~01456 to 0,1~5 Pascal), is applied Jo the told to cause the resin to encapsulate the filler The elevated temperature and ~uperatmospheric pressure are maintained for a time sufficient to partially cure the resin and form a unitary structure which can be ejected from the told. The ejected structure is then subjected to a further heaving cycle to completely cure the resin.
By the practice of the present invention, reinforced syntactic foam composites are obtained which have a coefficient of thermal expansion of about 25 x 10-6 in/in/F (45 x 10-~ cm/cm/C) or less anal a density of lets than loo gm/cm3, as well as long-term thermal stability, amenability to being molded in various configurations, end ability to meet the NASA outguessing requirements Using the preferred epoxy resin formulation described herein, composites are obtained which have a coefficient of I thermal expansion of about 9.0 10-6 in/in/F (160?
x 10 6c~cm/ I or loss. In addition, the mechanical properties of these composites are repealable.
hi combination of properties makes the composites of the prevent invention particularly jell suited for use as a ~ubstituts for aluminum in antenna and antenna microwave component used in space applications. In particular, heat curable epoxy resins comprised of mixtures of ~etrafunc~ional aromatic epoxy resins and liquid android when heated to 150F are sufficiently low in viscosity to accept loadings of micro spheres up to 65 percent of the volume of the system, fiber loadings of up to 10 percent, and bead loadings up to 55 percent.
These microsphereffiber/bead filled epoxy resins are readily curable and when cured produce Cenozoic foam composites having specific gravities of between 0.8 and 0.9 and coefficients of thermal expansion approximating - - -1 what of aluminum or twill depending ox the filler fiber volume used in the composite of the prevent invention, composites may be tailored to have coefficients of thermal expansion ranging from that of the unfilled resin to that of steel.
Because of their relatively low coefficient of thermal expansion, epoxy resin bass syntactic foam composites prepared in accordance with the present invention have been determined to by specially amenable I to conventional petal plating processes, such as elector-less plating when the surfaces thereof are prepared for plating by plasma treatment Thy relatively high adhesion of metal deposits to the surface of the present composite is believed to be a function of both the topography of the plasma-treated surface plus the mechanical integrity of the remaining surface The plasma remove the resin skyline from the composite, leaving the graphite fiber/microballoon Miller exposed, to provide a surface which is readily playable. Such petal plating of ha composite of the present invention may be required in forming antenna components in which an 21ectrically conductive surface or path is required, us is known in the art.
To effect plasma treatment in preparation for plating the surface of the filler reinforced epoxy resin based composite is subjected to a plasma process with a reaction gas containing a mixture of air, nitrogen, or arson with oxygen, water vapor, nitrous oxide, or other resin oxidizing source, to remove the polymer I Cowan and expose the filler, as discussed bevy.
Normal plasma etching conditions known to the art are used Fur example, for a plasma excitation energy of 200 watt~/ft2 of composite, an O2/in~rt gas source of approximately 1000 ml~minute, a vacuum pressure of 200 micrometers Hug, and one hour duration are used 1 When a silver deposit is required, us in an antenna ~aveg~ide structure, it is advantageous to first for a layer of an electroless or vapor deposited metal such us copper to provide a conductive surface which can then be built up with additional electrolytic plating such as copper or silver plate to produce a sooth surface finish. Electrolytic silver plating may readily be formed on the electrolytic copper surface to provide silver plated surface with Good adhesion to the underlying composite material.
Blectroless plating of the plasma-treated composite surface can be accomplished by standard procedures such as by dipping the plasma-treated composite in the plating solution for a time sufficient to achieve a continuous buildup ox metal on the etched surface. Metals that can be plated on the molded epoxy resin bayed composites prepared in accordance with the present invention include, for example, copper, silver, nickel cobalt, nickel/iron, nickel/cobalt, other nickel alloys, and gold. For electroless copper plating, an aqueous bath of Shipley I ~328 copper plating 801ution may be used, which contains copper ~ulfatet sodium potassium tart rate, an sodium hydroxide. Other electroless copper plating formulations can also be employed. The plating bath is agitated or stirred prior to immersion of the plasma treated composite. Preferred plating temperatures ore in the range of about 15C to about 95C about 59F to 20~F). Metal adhesion ox this electroless copper plating has been determined to be excellent even after exposure of the played composite to cycle of widely different temperatures as described in Examples 3 and 4 herein.

Lo 3 1 Next, copper playing it built up to any desired thickness on the electroless copper by known electrolytic plating methods, using commercially available electron deposit copper playing solution. Finally n electrolytic silver plate is formed to the desired thickness on the electrolytic copper plate by known methods using commercially available silver plating solution formula-Chinese Silver plating of a composite of the present invention is described in Example 5 The following examples illustrate but do no limit the prevent invention.

This example illustrates a process for forming one type of fiber-reinforced syntactic foam composite in accordance with one process embodiment of the present invention.
The components of the syntactic foam formulation designated ~S-61~ are shown in Table I. The following details regarding the components of S-61 apply to Table I.
a. MOE is a ~etraglycidyl ethylene dianiline manufactured by Cuba Geigy.
b. HOWE is a nadir methyl android hardener manufactured by Cuba Geigy.
c. BDMA is ben~yldimethylamine accelerator available from Eye. Roberts or Cuba Geigy.
d. D32/4S00 micro spheres are borosilicate micro spheres having a mean diameter of 75 micrometers a specific gravity of 0.32, and a compressive strength of 4500 psi, available from the EM Company 22 ~L23~
-e 0 YO-YO giber are graphite f gibers willed to a length of about lS0 micrometers and having a diameter of bout 8 r~icronieters, available from the Sullenness Corporation ., S f, ~R38S~ ~R55~ and ~R9S are tit2lnate coupling and wetting agents, available from Enrich Petrochemical tympany, Ennui, New Jersey.
y. AFT it a surfactant, available from Foreign Comma cay 1 Co .
lo TABLE I

__ _____. . _ .. .__ _ _ Component _ _ PHI* _ weight (Scrams) 1. Resin MOE epoxy resin 100 400 HOWE hardener 100 1.0 BDMA accelerator 0 . 25 4 . 0 CRUSOE 1.0 4.0 2 . Micro spheres 2 5 Do 2/4 5 0 0 0 . 3 1, 2 AFT (Optional) 0.2 0.8 3 . Fiber M i 1 led GYP 0 20 8 0 ~R9S

, *Pill it parts per hundred epoxy resin .

Y .

1 Pre~_ati~n_of Graphite giber The JOY rift fibers in continuous tow or were cut into lengths of approximately l,f8 inch to 1/2 inch ~0,32 Jo 1.27 centimeters using paper cutter.
Batches of the chopped fibers approximately 80 grays each) were loaded into a ball mill jar having a one-gallon capacity and sufficient Freon TO was added to cover the ceramic balls to serve as a suspension tedium.
The fibers were milled for 24 hours. Scanning electron micro graphs of toe milled fibers showed them to be broken into small fragments ranging from approximately 2 to 13 micrometers in length The milled fibers and Freon were poured into a shallow stainless steel pan, and the Freon was allowed to avapor~te. The fibers were then dried 4 hour in an air circulating oven set at 250~F (121C) and sifted on a vibration plate to pays a 325 mesh screen. The dried sifted fiber were stored in a desiccator box until ready for use.
Composite Formation The formulation S61 was prepared as follows. A
one-gallon hot/cold pot for a Waring blender was heated to 140DF (60~C) using a te~perature-controlled water bath. The remeasured amount of the HOWE hardener was put in the blender and the mixer speed was adjusted using a Voyeur variable potentiometer SO that thy hardener way just barely agitated. With the blender on Lowe setting, the Variac was turned to 70 percent of I full pod Thy resin which had been preheated Jo 160F (71C), was added to the pot an the contents of the pot were mixed until the mixture appeared homogeneous about 5 minutes); and then cooled to room temperature.

,3~3~

1 Next there was gradually added to the pot thy RR38S~
AFT tuitional, end 25 percent of the milled fibers which had been previously dried overnight in on oven at 200F SKYE and fluffed by running in the blender on Lowe speed at 70 percent of the full Variac speed for about 15 seconds for 5 grams of fiber. The mixture was mixed for about 5 minutes. text, 10 percent of the micro spheres which had been dried overnight in an oven at 200~F (93C) was gradually added and the contents of the pot were mixed until streak of micro spheres dupe-peered. The remaining amount of fiber and the Greece were gradually added and the pot contents mixed for about 30 minutes Next, the BDMA was added slowly, followed by the RR55 and the remaining amount of micro-sphere The pot contents were mixed until streaks omicro~pheres disappeared.
Then the pot was covered and a vacuum pump was attached to the pot with the pump set to pull vacuum of 22 inches (559 mm3 of mercury. The mixer was run for 45 minutes under vacuum or until there were no black streaks of fibers in the mixture. Finally, the mixture was carefully poured Jo as to minimize air entrapment, into a preheated stainless steel test specimen mold which had been prepared by cleaning with methyl ethyl kitten solvent, baking at 300F (149C) for 30 minutes, brushing with a fluorocarbon mold release agent to provide three coats of the release agent with 30 minutes air drying for each coat, and preheating to 140~F l60~C). optionally, the formulation was injected with an air gun into the mold) After pouring the mixture into the mold, the mold was vibrated on a vibrating table for 5 minutes at the maximum safe speed, with a large flat 0.5 inch thick aluminum plate placed on top of the mold. Next, the mold was placed in an oven preheated to 275~F (135~C) end a thermocouple was placed on/in each of the following. on the mold, in the oven, and in the mold contents through a hole in the wide wall of the mold. when thy therm couple in the mold contents registered 275F ~135C), the oiling cure cycle was run: 10 minutes at 275F
(135~C) 10 minutes at 300~F (149C); 120 minutes at 350F (177C). The maximum oven rate was used for changing temperatures The mold was removed from the oven and was disassembled, and the part was removed from the mold while the told was still hot, being sure to keep the thermocouple embedded in the sync tic foam. The part was~deflashed as necessary with a file. For the post-cure, the remolded part was placed in an oven preheated to 400F ~204C) between 0.5 inch thick aluminum plate, with 2-5 kilograms weight on the top plate. When the thermocouple in the syntactic foam registered ~00F
(204C), the following post-cure cycle was run: l hour at 400F (204C); 1 hour at 425F (218C); 1 hour at 450F (232C), and 1 hour at 475F ~246DC~ Finally, the part was removed from the oven.
The fiber reinforced syntactic foam composite formed as described above was found to have the properties I shown in Table II. With regard to Table II, the following test requirements apply:
a. CUTE was determined using a quartz dilatometer to measure the change in length as a function of temperature b. Specific gravity was measured using a pycnometer~
c. Viscosity was measured with a Brook field Viscometer~

I I

Id Shrinkage was assured by determining the dimensional difference Boone the molded Educate and the n~oldl, e. Gel time was determined qualitatively as I, the time required for the Lydia resin to - for a Mel f. Pot life spas determined qualitatively as the time required err he lugged resin to increase in viscosity to the punk of being unworkable.
9. Degree of exoth~rm way determined by using a differential scanning calorimeter.

TAB LYE I I

_ . . . _, _ Property Value . . I _ _ _ _ _ ._ _ _ __ _~_ CUTE 19-22 x 10-6 cm/cm/C
10c6-12.7 x 10-6 in/in/F
Specific gravity 0.80 Vacuity it 150F ~65.6"C) 35,000 centipoise Sir linkage 0 . 8 4 Gel tire It minutes Pot I fax >360 minute Degree of exotherm 15~ l 8 . 3C~

3~3~

This example illustrates a process for forming ~iber-reinforceq syntactic foam composites of various compositions in accordance with the pronto invention.
The components of the various fonnulations designated as the ~RSF series are shown in Tale III.
The owing detail regarding the specific components apply to Table IIIo a. Epoxy is a mixture of 70 part Glyamine 135 (diglycidyl ortho toluidins) and 30 parts Glyamine 120 (tetraglycidyl elan dianiline~, both materials obtained from FIX
Resin of San Francisco, California, Mixed with about 115 parts nadir methyl android hardener and about 0.25 parts ben~yldimethyl-aniline accelerator.
b. ZeeoRpheres 0/8 are solid glass spheres having a median diameter of 3 micrometers, available from elan Industries of SO Paul, Minnesota.
I Carbo~pheres Type A are hollow carbon spheres having an average diameter of 50 micrometers, available from Versar of Springfield, Virginia.
do EM A 32/2500 glass bubbles are glass micro-spheres having a mean diameter of 50 micro-peters) a specific gravity of 0.32, and a Compressive strength of 2500 psi, available from the EM Company of Minnesota.
e. EM A 16/500 are glass micro spheres having a mean diameter of 75 micrometers, 8p~cific gravity of 0.16, end a compressive strength ox 500 psi, available from the EM Company.
PO Eccospheres SO are hollow silica ionospheres having a diameter of 45-125 micrometers, available from Emerson and Curing Into of Canton, Massachusetts, 1 Graphic 213 R40 beads ore solid glass micro-spheres having dl~meter of 3~8 ~icrome~ers, available from ore co Inc. of Torrance, California ho EM S 50 (50~) are graphite fibers having a length of about 50 micrometers and a diameter of about 8 micrometer Mailable from Courtaulds Co. ox the United kingdom.
to AS 50 (250~) refloat ore graphite fibers having length of about 250 micrometers and a diameter of abut micrometer, available from Chortled of the United Random . aye ~MS-50 (1/16~) are graphite fiber having length of about 1600 micrometers and a diameter of bout B micrometer, available Finn and Pram of Sun Valley Cali~orni~.

Using each of the formulations of thy RSF errs 20 disowned in Table III7 a fiber reinforced syntactic foam composite way ford following the general procedure jet forth in Example 1. The properties of each of these composites it shown in Table IV. The following test requirement were applied or the Mormons in Table IVY

I

~3~7~

a . Density was determined by pycnometer O
b. CUTE was determined using a quartz dilato~neter to measure the change in length ( Al ) as function of typewriter .
c. Compr~sivS~ strength way determined using - the Arcane Society for Trusting end l~qaterial~ ~ASTM) 5t~ndard Noel D595 .
d. Compressive modulus was determined using STYMIE D695, using crosshead speed in place of train gouge.
e ., Ion format was determined by visual iLnspe~tion D
YE . Viscosity way measured with a rook issued Vi~cometer .

I
TABLE III
OOMP9SITIûN OF ~ORMUI.ATIONS lo RSF SERIES

VOLUME RATIO OF FOAM FILLERS
__ _ . _ MICRûSPHERE5 fibers _ .____ __ . _, I
Z TV o Us o o m I a _ or => -I _ _ ELI _ to :1: O Us Lo. I D- OX O Jo N U) Lo) I_ Jo c:, o O my j_ O LO I S" r Jo O I L-J I Lo a K
I I I I Lo ) I Q
__ __ _ __ 3 0.405 0~,098 0.~71 ~.025 4 O owe 5 0 01~48 0 . 514 O .064 O D40 1 O . 500 .0 59 O .040 0.4Ul 0.500 0.~59 O owe*
7 û.53~ 0.057 0.400 0.,007 ~.530 0.057 0.395 ~.~18 13 0.536 ~.057 0.400 0.007 I ID .530 .057 00395 O "~18 19 0,37 0.05 û.51 0.0~
O ~322 O oily O ~586 O ~050 I 0~375 00048 0~514 0006 23 1)D583 0~023' 0~36~ Oily ~25 O ion O ~022 O I 50 O ~025 26 0.583 0~.023 ~"368 IDEA
û.5~3 0.0~3 0.368 OKAY
29 ~83 O.g23 00368 00~26 31 0.496 0.0~2 0.4~7 0.025 33 O .!503 O owe O ~450 O ~0~5 34 0.39~1 0~026 Owe 0~030 OF O .410 O .025 O . 530 O .035 O .353 0.028 .588~ O .û32 36 0.383 0.026 __ 0.560 0.031 __ Plus 0~007 of AS 50 ~250 ) graphite _ EM Aye used on place of Aye 31 ~.23 TABLE I V
PAPACIES OF COMPOSITES OF ~ORMllLATIONS OF RSF SERIES

__ _ _ . _ . pa. I
I_ Lo . I I_ Jo Jo I.) C to z _ h _ ___ , ._ _ 3 ~.8~8 16 ~82 1~,300 394 3 .7 5 4 û.881 13.81 16 Noah 447 4 I
O .87~ 15.10 I ,40~ ~û6 4 .0 6 0.869 22 .16 14 ~300 407 3.5 5 7 O.g68 20 Jo 15,100 394 2 .7 8 0.982 21 .39 18,400 ~10 4.7 7 13 1.00~ 25.46 guy 386 203 7 14 1 .019 25.55 15,40û 405 1 98 6 19 0.852 14 .06 13 ,200 411 4 .0 3 0 .694 14 .09 B9600 335 2.7 2 21 D~,8561 17 .0214 ,000 439 3 .. 4 3 23 0 .9912 20 .6916 ,300 384 5 . 5 7 1.0387 30 . 51 19 DOOR ~23 __ 6 26 1 .005 21 .7315,700 395 7 .3 5 I 0.982 20.1017,1~ 411 6.5 29 1 .002 2û.7017 ,800 393 7 .6 5 31 0.~88 23 .9017 ,800 400 6 .6 8 33 0.815 23,~0~3,300 343 3.9 7 34 0.824 14.~917,~00 39~ I 6 34F D 842 14.Z417,300 425 I_ 0 738 17.2310>200 303 4~,0 6 36 0.7~5 17 .1~12 ,100 335 3 .0 5 1 put 1.45 x 10-4 Pascal , . . _ . . _ This example illustrates the formation of a fiber-reinforced syntactic foam composite using the preferred epoxy resin formulation and preferred vacuum liquid transfer lying prows described herein.
Thy heat curable epoxy resin formulation hod the hollowing positions Resin Component Diglycidyl orthotoluidine 100 ~adic methylanhydride 100 2-ethyl-4-~ethyl imidazole 2 This composition had gel time of 25 minutes, visc05ity of 220 centipoise at 75F (24C)~ end a CUTE of 30.8 to 32.3 x 10-S in/in/F (55.8 to Sol x 10-6 cm/cm/C)7 A filler mixture was prepared having the composition shown below and density of 0.543 gm/cm30 Sarbospheres are Hoyle carbon ~icroballoons having a mean diameter of about 50 micrometers, available from erasure Inc. of Springfield, ~irg1nia. MY graphite fiber ore graphite fibers having length of about 50 micrometers available from Courtaulds Co. of the United ~in~dom. Titan ate icing agents ore available from Enrich Petrochemical Co. of Bayonne, New Jersey.

I

~Lq~3~

n 11- r giddily WHITEHALL
-Carbo3phere9 50 micrometers I
HUMS fiber, 50 micrometer 50 Titan ate sizing gent ~R~38M
Using the bunted resin and filler, each of a series of resin/filler formulations shown in Table V
was processed as described below in order to form the composite of the present invention The filler composition it a mixture of the fiber and microphone pretreated with the sizing agent us previously described herein) aye loaded into a cleaned I inch x 0.5 inch ~14cm x 1.3cm) wide slab told internally coated with a polyvinyl alcohol release agent The mold was preheated to 212F (100C), the temperature at which hardening of the heat curable epoxy resin formulation was initiated. The epoxy resin formulation was poured into the told containing the filler. The mold was placed in a laminating press, a nylon vacuum bag was constructed around the compression tooling of the press, and a vacuum pressure of 125 millionaires mercury pressure (166~625 Pascal) was maintained on the assembly for 2 minutes to draw down the resin to impregnate the filler and to degas the resin aerial in the mold The vacuum way then released without removal of the vacuum bay and the assembly held in this passive vacuum state for an additional 2 minutes Thereafter, a constant positive 33 prowar of approximately 800 pounds per square itch (41,360 mm Hug or 5.5 x 106 Pascal) way impost on the rein filler mixture in the told for 2 hours at 212F
(100C~. During this pressurization stage, the resin was bled from the mold in the amount noted in Table V.

I:, 1 The molded composite slab ha sufficient Green strength to be ejected from the molt thereafter it was post cured for 4 hours unrestrained, in an oven jet 300~
~149C). The final ~oid-free slab contained the filler ratio noted in Table V and was cut into appropriate shapes for physical testing. The composite was found to have the physical properties which are summarized in Table Yip As indicated by the values for CUTE given in Table VI, unexpected significant improvement in the CUTE
of these composites was obtained using the preferred resin composition and filler compositions described herein.
In ~ddltion, a typical sample was tested in accordance with ASTM E-595-77 end found to have collected volatile condonable material (CVCM) of less than 0.1 percent and a total sass 1055 (TML) of less than 1 percent, which meets the NASA outguessing recurrent.
Further, for Specimen 1 of Table V, a portion of the molded slab was surface plated with copper by subjecting the surface of the slab to on oxygen rich plasma tzeat~ent, as previously described. the treated slab was then dipped into Shipley #328, electroless copper plating solution, as previously described, and then dried at 248~F (120C3 under 29 inches (737mm) Hug (gauge prowar The plated composite was then evaluated for adhesion ox the deposited copper layer using an STYMIE
D3359 tape Dunn text before and Tory 25 Swiss of I thermal shock imposed on the plated surface by alternately dipping the plated specimen in liquid nitrogen (~320F
or -196~C) or 30 seconds and boiling water (212F or 100C) for 10 seeondsD No loss of copper was observed.

TABLE V
COMPONENTS OF MOLDING COMPOSITE
_ . ___ ___ Bleed During specimen Resin Filler filler Ratio Molding No. my (gyms,) (it-%) vowel %
_ _ ._ . __ 2 30 9.4 3B 57 47.8 3 30 9.4 38 57 ~7.9 4 17.0* So 37 I 45.3 19.0* I 39 59 5~).6 6 20.7~ I 41 60 5~6 _ _ _ RR134S sizing agent was substituted for the previously noted icing agent.
We Resin bleed 100 where We initial resin weight We resin displaced from the told, using bleeder cloth.
VQ1 . calculated from resin bleed varies about 10-20% of the actual vol. 4 value.

- I
I

TABLE VI
PHYSICAL PROPERTIES OF MOLDED COMPOSITES

I_ . .
Specimen Thickness lunate CUTE*
NOD- ( in, gm~cm~ 10-6 cm/cm/~C
(l0''5 in~in/F~

1 0.J,78 ~743 6.6 (3.6 ~.~50 ~u900 16.2 ~9.0~
3 0.565 0~B76 14~2 (8.1) 1.070 û.~89 __ 1 .0~2 0.915 __ 6 1.065 0,~14 _ . _ Determined using a quartz do latometer .

I

EXAMPLE
__ this example illustrates the formation of composites jet forth in Example 3 with the exception that the composition of thy filler formulation was arrowhead. The procedure cot forth in example 3 was followed except that the filler compositions shown in Table VII were used, Tile following details regarding the pesky opponent apply to Table VI I O
a. Carbospheres are carbon ionosphere having a specific gravity of 0.32 end 21 mean diameter of 50 ~icromet~rs, available from Varier Corporation .
b . f3M-S 50 501J ) graphite f gibers are graphite f giber heavenly a length of about 50 ~nicromet~rs and I diameter of about 8 micrometers, available from the Courtaulds Co. of the United Kingdom.
c . lJ4 on ITS 50 graphite f gibers are graphite leers having a length of bout 250 micrometers and a diameter of about 8 micrometer available from the Courtaulds Co. of the United Kingdom.
do ~::15/250 glass micro balloon are keypad I
boro~ilic:ate glues have a diameter of 10-2~0 micrometer a density of 0.15 gm~cm3, and a compressive strength of 250 psi, available from the EM Company of Minnesota.

The physical properties of the molded composite slabs Jo f orbed ore jet forth in Table VIII .

I

_~___ _ In C , , I, _ I_ I:
_, _, X _ Eye N 0 . I
__ _ I_ I
O 1:
Us I Ox 0 I_ 11'~ as v ~~
O _ o _ I

I I I h - I
I . _ 4 Go e o I_ Us In us P Us æ
C
a) o ED
Cal 6Q I o o U YE:
- -I-to co I
-o -- ----I o I

TWILL try I I
PHYSICAL PP~t:)PERTXES OF MOLDED COMPOSITE: ~I.AB5 Fly tie r . _ _ _ _ _ S Used i n Pies i n Cut Melded Thickness density Filler Ratio bleed Coatirag Sample ( in. (gm/cm3 ) (Wit go ) (Vow .% ) Removed . __, . ,, ,, .- _ __ _ 3 1.0~0 39 5g 51.0 < 5%
B 02540 0.75326-~7 56-77 ~1.9 < 5%
C O ~35~) to .90.8 27 5~1 16 ox 5-15~6 _, _ _ _ _ I In addition, the surfaces of the molded composite slab of Table VIII were then subjected to plasma treatment under the following conditions: Inert gas Source of approximately Lowe ml/minute, vacuum pressure of 200~ Hug, and one hour duration. The surfaces of the plasma etched lobs were then copper plated to a thickness of bout 3-4 m$1s by dipping the itched slabs in an aqueous Shipley ~328 elec~roless copper plating be h.
the plated composite was then evaluated for adhesion ox thy deposited copper layer using the AUTUMN
D3359 tape adhesion test and thermal shock cycle of Example I The adhesion results are recorded in Table VOW indicating the amount of copper coating on lattice removed by the tape.

i:

EXPEL S
A Syntactic foam composite prepared from Specimen No. 2 of Table V described in Example 3 and molded in slab told was plated with silver as OOZED The surface of the slab way subjected kiwi an oxygen rich . -plasma etch which resulted in the removal of the surface polymer Skin, previously described " The etched slab was then metallized using the Shipley Company ~3~8 electrodes copper plating solution process, as previously described, and thoroughly resoled and dried at 243~F ~120~C~ under 29 inches ~725 Lyon) Hug (gauge pressure I, to provide a layer of electroless copper 20 l3icr~inches ~5.08 x 10-5 cm) thick. Next, the slab was immersed in an acid copper electrolytic plating path it 25~C ire 25 minutes to own on electrode posted copper layer 100 micro inches t2~.54 x 10-4 cm) thick.
Finally, the copper-plated slab was immersed in an electrolytic silver plating bath at 25C for 25 minutes to form a layer of silver 300 micro inches 7 .62 x 10 4 cm) thick .
. The ~ilver-platad slab way then evaluated for adhesion of the deposited layer using an ASP D3359 tape adhesion test before and after 25 cycles of thermal shock i~npo~e~d on the plated surface by al~cerrlately dipping the plated specimen in liquid nitrogen 1-328F
or -196C) ire one minute and boiling water ( 212F or 100C) for one minute. No adhesion lost of silver was observed I, The lover plated syntactic foam had the tame low 3Q Rough lo corrector a aluminum when tested for insertion lows it 4.6 joggers using standard electronic Tut o Thus, with the use of proper tooling cry molding, antenna wave guide tractor may be formed from the compute of the present invention, which are effective microwave so antenna component and which heel thy I
I

requirements for use in space ~pplic~tiorls,. syntactic essay played eslth metals such a silver end copper may serve us Dllet~l-plated core rural for both rove colaponents and microwave reflector.
S The fiber reinforced syntactic foam composes of the prevent invention achieve a 3-to-1 reduction in weight in comparison with aluminum, which makes eye component attractive for weight sensi~ivs applications in a spaceer~ft envirorlment~ At the tame lime, however, in situations calling for high volume production, the readily moldable nature off the reinforced foam mixture disclosed herein further officer the potential of iguana-f scantly reduced cot in comparison with the machining traditionally employed for the production of conventional metal parts.
The preceding description has presented in detail exemplary preferred ways in which the concepts of the present invention may be applied Those skilled in the art will recognize that numerous alternatives encompassing Ryan variations may readily be employed without departing prom the intention and cope of the invention jet forth in the appended claims . In particular, the present inventor is not limited to the pacify resin, fiber or }nicroballoons set forth herein a example., By iEollowing the teachings provided herein relaying to the of fact of etch component of the mixture on the f net composite and the effect of the various component on etch Thor other suitable resin, fiber, and micro balloon materials my readily be determined Further, by I following the teachings provided her D it ray be determined how to form composite materials having a density or Coffey iciest of thermal expansion other than Thea en f oath herein as required for thy specifically mentioned end use in space applications.

,:

Claims

What is Claimed is:

1. A fiber-reinforced syntactic foam composite having a specific gravity less than 1.0 and a coefficient of thermal expansion of about 25 x 10-6 in/in/°F
(45 x 10-6 cm/cm/°C) or less, the composite being prepared from an admixture comprising a heat curable thermosetting resin, hollow microspheres having a diameter in the range of about 5 to about 200 micrometers and fibers having a length less than or equal to 250 micrometers.

2. The composite of Claim 1 wherein the resin comprises a material selected from the group consisting of an epoxy, a polyester and a condensate of formaldehyde.

3. The composite of Claim 2 wherein the heat curable thermosetting resin comprises a mixture of an epoxy resin and a polyfunctional curing agent.

4. The composite of Claim 3 wherein the epoxy resin is tetraglycidyl methylene dianiline, a mixture of diglycidyl orthotoluidine and tetraglycidyl methylene dianiline, the diglycidyl ether of Bisphenol A, or a phenol formaldehyde novolac polyglycidyl ether.

5. The composite of Claim 3 wherein the polyfunctional curing agent is a polyamine, polycarboxylic acid anhydride, or the maleic anhydride adduct of methyl cyclopentadiene.

6. The composite of Claim 3 wherein the mixture further comprises benzyldimethylaniline as an accelerator.

7. The composite of Claim 1 wherein the hollow microspheres are formed of glass, silica, carbon, acrylate resins, or phenolic resins.

8. The composite of Claim 7 wherein the hollow microspheres are formed of glass and have an average diameter of about 50 micrometers.

9. The composite of Claim 7 wherein the hollow microspheres comprise a mixture of glass microspheres and carbon microspheres.

10. The composite of Claim 1 wherein the fibers are formed of graphite, glass, carbon, nylon, or polyamide.

11. The composite of Claim 10 wherein the fibers are formed of graphite and have a length of about 50 micrometers and a diameter of about 8 micrometers.

12. The composite of Claim 1 wherein said admixture further includes a coupling and wetting agent.

13. The composite of Claim 1 wherein the admixture further includes solid microbeads.

14. The composite of Claim 1 which comprises about 35 to about 65 percent by volume microspheres and about 3 to about 10 percent by volume fibers, the balance being a matrix comprised of the heat cured resin throughout which the microspheres and fibers are dispersed and bonded together.

15. The composite of Claim 14 which additionally comprises about 2 to about 8 percent by volume of solid microbeads having a diameter of about 2 to about 8 micro-meters.

16. The composite of Claim 1 wherein:
a) the heat curable thermosetting resin comprises a mixture of diglycidyl orthotoluidene, tetraglycidyl methylene dianiline, nadic methyl anhydride, and benzyl-dimethylaniline;
b) the hollow microspheres are glass microspheres having a mean diameter of 50 micrometers;
c) the fibers are graphite fibers having a length of about 50 micrometers and a diameter of about 8 micro-meters; and d) the admixture further comprises solid glass microbeads having a median diameter of 3 micrometers.

17. A fiber-reinforced syntactic foam composite as set forth in Claim 1, comprising:
a) a heat curable thermosetting epoxy resin comprising a mixture of tetraglycidyl methylene dianiline, nadic methyl anhydride, and benzyldimethylaniline;
b) hollow glass microspheres having a mean diameter of about 75 micrometers; and c) graphite fibers having a length of about 150 micrometers and a diameter of about 8 micrometers.

18. An article of manufacture comprising a body formed from the composite material of Claim 1.

19. The article of manufacture set forth in Claim 18 which further comprises a layer of electrically conductive material adhered to selected surfaces of the body.

20. The article of manufacture set forth in Claim 19 wherein said article comprises a component in an antenna structure.

21. A method for fabricating a fiber-reinforced syntactic foam composite as set forth in Claim 1, which comprises the steps of:
a) admixing a heat curable thermosetting resin, hollow microspheres having a diameter in the range of about 5 to about 200 micrometers and fibers having a length less than or equal to 250 micrometers to form a mixture of the resin, microspheres and fibers; and b) curing the mixture of the resin, microspheres, and fibers in a mold of predetermined geometry to a thermoset state to provide a composite structure contain-ing about 35 to about 65 volume percent microspheres and about 3 to about 10 volume percent fibers dispersed throughout the resin matrix, and the resin comprising the balance of the composite, wherein the composite has a specific gravity of less than 1.0 and a cofficient of thermal expansion of about 13 x 10-6 in/in/°F (23 x 10-6 cm/cm/°C) or less.

22. The method of Claim 21 wherein the admixing comprises:
a) forming a liquid dispersion of the microspheres and fibers in a coupling agent;
b) filtering the dispersion to separate the micro-spheres and fibers from the liquid as a filtration residue;
c) drying the residue to provide a mixture of microspheres and fibers coated with the coupling agent;
and d) admixing the coated microspheres and fibers with the resin.

23. The method of Claim 22 wherein:
a) the microspheres are hollow glass microspheres;
b) the fibers are graphite fibers, c) the coupling agent is selected from the group consisting of a silane compound and a titanate compound.