JPS6193404A - Carbon fiber reinforced plastic mirror - Google Patents

Carbon fiber reinforced plastic mirror

Info

Publication number
JPS6193404A
JPS6193404A JP21494584A JP21494584A JPS6193404A JP S6193404 A JPS6193404 A JP S6193404A JP 21494584 A JP21494584 A JP 21494584A JP 21494584 A JP21494584 A JP 21494584A JP S6193404 A JPS6193404 A JP S6193404A
Authority
JP
Japan
Prior art keywords
coating layer
mirror
cfrp
substrate
metallic coating
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP21494584A
Other languages
Japanese (ja)
Inventor
Kenzo Kadotani
門谷 建蔵
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Resonac Corp
Original Assignee
Hitachi Chemical Co Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hitachi Chemical Co Ltd filed Critical Hitachi Chemical Co Ltd
Priority to JP21494584A priority Critical patent/JPS6193404A/en
Publication of JPS6193404A publication Critical patent/JPS6193404A/en
Pending legal-status Critical Current

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  • Optical Elements Other Than Lenses (AREA)
  • Laminated Bodies (AREA)

Abstract

PURPOSE:To obtain a CFRP mirror having less tendency to absorbing a moisture in an atmosphere of air at a room temp., thereby less releasing a gas in a vacuum by forming a metallic coating layer for preventing the moisture absorption over a whole surface of the CFRP substrate. CONSTITUTION: The titled mirror is prepared by coating the CFRP substrate with the metallic coating layer and by providing a mirror surface of a vapor- deposited aluminum layer 4 which is transcribed on a concave side by an adherent 3 and also by providing a black coating layer 5 on a back of the mirror to cover a glossiness of the metallic coating layer 2 and to accelerate an absorption and a radiation of a radiant heat. The metallic coating layer is formed by chemical plating a metallic nickel and cupper etc. or by dipping the preheated CFRP substrate plate in a molton metal composed of a low melting point metal and then lefting it. If the CFRP substrate plate is sufficiently dried before forming the metallic coating layer on the substrate, the generation of gas is small in a space chamber, thereby making the vacuum easy for a short period.

Description

【発明の詳細な説明】 (産業上の利用分野) 本発明はカーボン繊維強化プラスチック(CFRP)ミ
ラーに関する。
DETAILED DESCRIPTION OF THE INVENTION Field of the Invention The present invention relates to carbon fiber reinforced plastic (CFRP) mirrors.

(従来技術) 地上において宇宙環境を模擬する実験室(スペースチャ
ンバー)内に置かれ、窓から投入した光を当て、これを
反射して均一な平行光にするための、コリメータミラー
は一定の曲率半径を有する凹面ミラーである。直径が3
m以上の大型ミラーになると、単体のミラーをつくるの
が困難であるから、六角形状の小ミラーを複数個、すき
まなく並べて大型ミラーを構成する。例えば直径が10
m程度の大型ミラーでは、小ミラーを100個近く並べ
て構成することになる。
(Prior technology) A collimator mirror is placed in a laboratory (space chamber) that simulates the space environment on the ground, and has a certain curvature to reflect light from a window into uniform parallel light. It is a concave mirror with a radius. diameter is 3
When it comes to a large mirror of m or more in size, it is difficult to make a single mirror, so a large mirror is constructed by arranging a plurality of small hexagonal mirrors without gaps. For example, the diameter is 10
A large mirror of approximately 100 m in size would be constructed by arranging nearly 100 small mirrors.

従来このようなミラーは、アルミ合金を基板として、こ
れにニッケルをメッキして研摩してから。
Conventionally, mirrors like this are made using an aluminum alloy as a substrate, which is then plated with nickel and polished.

鏡面としてアルミを蒸着していた。この金属ミラーでは
、小ミラーを1個ずつ研摩して仕上げる必要があシ、製
作に長期間を要し、また高価であった。さらにスペース
チャンバー内は、暗黒時には−200℃近くになシ、照
光時にはミラー表面が+100℃近くな9.温度変化の
幅が非常に大きい。そこでアルミ合金(線熱膨張率が約
25×10−’+m/an’c)の小ミラーを組合せて
構成する場合に、最高温度(約100’C)で間隙を0
にしても、最低温度(約−200℃)では約0.75%
の間隙が生じる恐れがある。このように間隙ができると
、平行光の均一性が悪くなシ、また小ミラーの端面に光
が当シ、散乱して温度上昇をひき起こすもとになる。
Aluminum was vapor-deposited as a mirror surface. With this metal mirror, it was necessary to polish and finish each small mirror one by one, which required a long period of time to manufacture and was also expensive. Furthermore, the inside of the space chamber is close to -200℃ when it is dark, and the mirror surface is close to +100℃ when illuminated9. The range of temperature changes is very large. Therefore, when combining small mirrors made of aluminum alloy (linear thermal expansion coefficient of about 25 x 10-'+m/an'c), the gap can be reduced to 0 at the maximum temperature (about 100'C).
However, at the lowest temperature (approximately -200℃) it is about 0.75%
There may be gaps. If such a gap is formed, the uniformity of the parallel light will be poor, and the light will be scattered on the end face of the small mirror, causing a rise in temperature.

そこで線熱膨張率(沿面方向)がほとんど0である(実
測では1 x 10−’ a+/m”c以下)。
Therefore, the coefficient of linear thermal expansion (in the creeping direction) is almost 0 (according to actual measurements, it is less than 1 x 10-'a+/m''c).

CFRPを基板とするミラーが提案されている。Mirrors using CFRP as a substrate have been proposed.

CFRPの小ミラーを組合せて構成する場合には。When configuring a combination of small CFRP mirrors.

室温付近で間隙Oに設定すれば、高温でも低温でも間隙
はほとんど生じないのである。しかしCFRPミラーの
問題点の一つは1表面に光反射率のよい鏡面を形成する
のが難しい点にある。すなわちCFRP面、あるいはこ
れに合成樹脂のトップコート被覆層を塗布して、これを
研摩しても傷がつき易いので、その上に蒸着したアルミ
鏡面がきれいにできない。
If the gap is set to O near room temperature, almost no gap will occur at either high or low temperatures. However, one of the problems with CFRP mirrors is that it is difficult to form a mirror surface with good light reflectance on one surface. That is, even if a CFRP surface or a top coat layer of synthetic resin is applied to the surface and polished, it is easily scratched, and the aluminum mirror surface deposited thereon cannot be cleaned.

もちろんアルミ合金ミラーと同様に、CFRPにニッケ
ルメッキし、この硬い面を研摩してアルミ蒸着してもよ
いが、従来のミラーと同様の手間がかかる。発明者らは
先に、CF几P基板に良好な鏡面を能率的に形成する方
法を開発した。これは「転写法」と称し、まず研摩した
ガラスないしは金属製の盟を用意し、この表面にアルミ
蒸着層をもうけておく。次に、CFRP基板または型に
好ましくは無溶剤形の接着剤を塗布して1両者を合わせ
、接着剤を硬化させてから離型すると、アルミ蒸着層が
CFRP基板側に転写され、良好な鏡面ができる。この
方法では、正確に研摩した型が一つあれば、転写ができ
、またCFRP基板とアルミ蒸着層の間は接着剤がつま
るので、CPRP基板凹面の刀ロエは荒くてよい。ある
いは研摩した盤とほぼ同一形状で1表面は荒くてもよい
金属を用いてCFRP基板を成型しておけば、その表面
を接着をよくするためサンドペーパーで荒らすでいとで
、転写を行なうことができ、能率的である。
Of course, like aluminum alloy mirrors, CFRP may be plated with nickel, this hard surface polished, and aluminum deposited, but this requires the same effort as with conventional mirrors. The inventors have previously developed a method for efficiently forming a good mirror surface on a CF-P substrate. This is called the ``transfer method,'' and first a polished glass or metal blade is prepared, and an aluminum vapor-deposited layer is formed on its surface. Next, a preferably solvent-free adhesive is applied to the CFRP substrate or the mold, the two are put together, the adhesive is cured, and the mold is released. The aluminum vapor deposition layer is transferred to the CFRP substrate side, creating a good mirror surface. I can do it. With this method, only one accurately polished mold is required for transfer, and since the adhesive is clogged between the CFRP substrate and the aluminum deposited layer, the concave surface of the CPRP substrate does not need to be roughened. Alternatively, if a CFRP substrate is molded using a metal that has almost the same shape as the polished disk and one surface may be rough, then the surface can be roughened with sandpaper to improve adhesion, and transfer can be performed. efficient and efficient.

しかしCFRPを基板とするミラーの、もう一つの問題
点はガス放出である。すなわち、一般に室温大気中に長
時間開放したCFRPミヲーは。
However, another problem with CFRP-based mirrors is outgassing. In other words, CFRP materials are generally exposed to room temperature air for long periods of time.

スペースチャンバー内に置かれたとき、いつまでも水分
を放出しつづけ、チャンバー内が所定の真空度(I X
 10−’Torrのオーダー)に達するのに、長時間
を要することになる。
When placed in the space chamber, moisture will continue to be released forever, and the chamber will maintain a predetermined degree of vacuum (I
(on the order of 10-'Torr) will take a long time.

(発明の目的) 本発明は、室温大気中に開放しても吸水しに〈<、シた
がって真空中でのガス放出が少なく、かつガス放出が短
時間に行なわれるように、jラー基板の温度コントロー
ルができるようにした。
(Purpose of the Invention) The present invention provides a flexible substrate that absorbs water even when exposed to the atmosphere at room temperature. The temperature can be controlled.

CFRPミラーを提供することを目的とする。The purpose is to provide a CFRP mirror.

(発明の構成) 本発明は、CFRP基板の全表面に金属被覆層をもうけ
、この表面の鏡面側にはアルミ蒸着層を転写し、裏面に
は黒色被覆層をもうけてなるカーボン繊維強化プラスチ
ックミラーに関する。
(Structure of the Invention) The present invention provides a carbon fiber reinforced plastic mirror in which a metal coating layer is provided on the entire surface of a CFRP substrate, an aluminum vapor deposition layer is transferred to the mirror side of this surface, and a black coating layer is provided on the back surface. Regarding.

アルミ蒸着層の転写は、前述の転写法によって行なわれ
る。
Transfer of the aluminum vapor deposition layer is performed by the transfer method described above.

第1図は本発明のCFRPミラーの一例を示す縦断面図
である。CPRP基板1は金属被覆層2に囲われている
。その凹面側は接着剤3によって転写したアルミ蒸着層
4の鏡面をもうけ、裏面には、金属被覆層2の光沢をか
くシ、裏面のふく射熱の吸収と放散を良くするため、黒
色被覆層5をもうけている。
FIG. 1 is a longitudinal sectional view showing an example of the CFRP mirror of the present invention. The CPRP substrate 1 is surrounded by a metallization layer 2 . The concave side has a mirror surface of the aluminum vapor deposited layer 4 transferred with adhesive 3, and the back side has a black coating layer 5 to hide the luster of the metal coating layer 2 and improve the absorption and dissipation of radiant heat on the back side. It's profitable.

CFRP基板1は一般に、カーボン繊維基材を積層し、
熱硬化性樹脂組成物を含浸硬化して得る。
The CFRP substrate 1 is generally made by laminating carbon fiber base materials,
Obtained by impregnating and curing a thermosetting resin composition.

金属被覆層2は一般に、ニッケル、銅などを化学メッキ
するか、あるいは低融点合金を溶解しておき、予熱した
CFRP基板を浸漬し引上げて形成する。このとき、低
融点合金とCFRP表面のぬれを良くするため、CFR
P表面にあらかじめ薄く、銅やニッケルをメッキすると
よい。低融点合金としては、an、37Pb(融点18
3℃) * Bs 142Sn(138℃)、In、5
0Sn(125℃)、Bi。
The metal coating layer 2 is generally formed by chemically plating nickel, copper, or the like, or by melting a low melting point alloy, dipping a preheated CFRP substrate, and pulling it up. At this time, in order to improve the wetting of the low melting point alloy and the CFRP surface,
It is best to plate the P surface with a thin layer of copper or nickel in advance. Low melting point alloys include an, 37Pb (melting point 18
3℃) *Bs 142Sn (138℃), In, 5
0Sn (125°C), Bi.

4+pb(124℃)などが手ごろである。黒色被覆層
5は、カーボン繊維基材に合成樹脂組成物を含浸して貼
付けるとか、カーボンを充填した合成樹脂塗料を塗布す
ることで形成できる。
4+PB (124°C) is reasonable. The black coating layer 5 can be formed by impregnating and pasting a carbon fiber base material with a synthetic resin composition, or by applying a carbon-filled synthetic resin paint.

金属被覆層2の厚さは、CFRP表面にでたカーボン繊
維(太さ7〜10μm)の突起を完全におおい、tたそ
の厚さが約50μmをこえると。
The thickness of the metal coating layer 2 is such that it completely covers the protrusions of carbon fibers (thickness: 7 to 10 μm) on the CFRP surface, and the thickness exceeds about 50 μm.

CFRPとの熱膨張差で、温度変化(−2006C〜+
100℃)のくり返しによって、はくりが生じ易いので
、15μm〜5011mの範囲が好ブしい。この程度の
厚さは、化学メッキではメッキ液に浸漬する時間を加減
して自由に得られる。また低融点合金の場合は、浸漬己
度を刀Ω減して自由に得られる。
Due to the difference in thermal expansion with CFRP, temperature changes (-2006C to +
Since peeling is likely to occur due to repeated heating at 100° C., a range of 15 μm to 5011 m is preferable. In chemical plating, this level of thickness can be freely obtained by adjusting the immersion time in the plating solution. In the case of low melting point alloys, they can be obtained freely by reducing the degree of immersion.

本発明のCF RPミラーにおいては、CFRP基板1
の全表面を金属被覆層2がおおっているので、金属被覆
層を形成する前に、CFRP基板を十分に乾燥しておけ
ば、スペースチャンバー内でのガス放出が少なく、シた
がって、短時間に真空度をあげられる。また鉄面には点
色被覆層5があるので、高真空中でも、チャンバー壁の
温度を変化させることにより、ふく射によってCFRP
ミラーを裏面から刀口熱ないしは冷却を行なうことがで
きる。すなわち、チャンバー内を早く高真空にして運転
を開始したいときは、加熱(ベーキング)してガス放出
を速めるとよい。また高真空で光照射中にCFRPミラ
ーの偏置上昇をおさえるには。
In the CF RP mirror of the present invention, the CFRP substrate 1
Since the entire surface of the CFRP substrate is covered with the metal coating layer 2, if the CFRP substrate is sufficiently dried before forming the metal coating layer, there will be less gas released in the space chamber. The degree of vacuum can be increased. In addition, since there is a spot-colored coating layer 5 on the iron surface, even in a high vacuum, by changing the temperature of the chamber wall, CFRP can be formed by radiation.
The mirror can be heated or cooled from the back side. That is, if you want to quickly create a high vacuum inside the chamber and start operation, it is recommended to heat (baking) to speed up gas release. Also, to suppress the eccentric rise of the CFRP mirror during light irradiation in a high vacuum.

冷却すればよい。Just cool it down.

(実施例) 次に実施例をのべる。実施例はモデル試料によυガス放
出量を比較した。鏡面の有無はとくに影響しないので、
CFRP基板に金属被覆層と黒色被覆層をもうけた場合
(実施例)ともうけない場合(比較例)を比較した。
(Example) Next, an example will be described. In the example, the amount of υ gas released was compared using a model sample. The presence or absence of a mirror surface has no particular effect, so
A comparison was made between a case where a metal coating layer and a black coating layer were provided on a CFRP substrate (example) and a case where a metal coating layer and a black coating layer were not provided (comparative example).

CFRP基板は、平織カーボンクロス(東し。The CFRP board is made of plain weave carbon cloth.

トレカφ6343 )を18枚重ねて、厚さ4mm1で
プレスし、脂環式エポキシ樹脂組成物(U3O社のj1
″iI環式エポキシ樹脂E凡L4221.100部、ヘ
キサハイドロ無水フタル酸90部、ベンジルジメチルア
ミン1部を配合)を、70℃、o、oiTorrで減圧
含浸したのち、大気圧下で120°0゜3時間、嘔らに
160℃、5時間かけて硬化した。
18 trading cards (φ6343) were stacked and pressed to a thickness of 4 mm, and alicyclic epoxy resin composition (U3O's j1
"iI cyclic epoxy resin E 4221.100 parts, hexahydrophthalic anhydride 90 parts, and benzyldimethylamine 1 part) was impregnated under reduced pressure at 70° C., OiTorr, and then impregnated at 120° C. under atmospheric pressure. It was cured at 160°C for 3 hours and then at 160°C for 5 hours.

実施ガでは、大きさ30cm角のCFRP基板に。In the implementation, a 30cm square CFRP board was used.

まずニッケル化学メッキ層を厚さ5μmはどこし。First, the thickness of the nickel chemical plating layer is 5 μm.

次に160℃、12時間乾燥したのち、低融点合金+ 
Bi t 428nを160℃で溶融した中に浸漬し引
上げて、厚さ25μmの金属被覆層をもうけた。次にこ
の片面に、カーボン扮を硅酸ソーダ(水ガラス)に添加
して塗布し、厚さ5μmの黒色被覆層を形成した。比較
例では、CFRP基板をそのまま用い、160℃、12
時間乾燥して条件を合せた。いずれも乾燥後に、約20
℃、70SRHの室内に1力月放置してから測定に入っ
た。
Next, after drying at 160℃ for 12 hours, the low melting point alloy +
Bi t 428n was immersed in a melt at 160° C. and pulled up to form a metal coating layer with a thickness of 25 μm. Next, a carbon layer was added to sodium silicate (water glass) and applied to one side to form a black coating layer with a thickness of 5 μm. In the comparative example, the CFRP substrate was used as it was and heated at 160°C and 12
After drying for a while, the conditions were adjusted. Approximately 20% after drying
After leaving it in a room at 70 SRH for one month, measurements were taken.

測定は、小型真空チャンバー内において、ガス放出量(
単位表面積当り)の時間変化をみた。第2図にそれを示
す。Aは比較例のCFRP基板であり、Bは実施例のC
FRP基板である。いずれも室温において測定した結果
である。実施例は比較例に比べてガス放出量が少なく、
より早く高真空に達するものと思われる。次にB′は実
施例のFRP基板の裏面から20cm離れた位置に、温
度80℃の熱板を平行に配置した場合で、板の温度は約
73℃となり、Bに比べて脱気の初期のガス放出が盛ん
となシ、脱気後3時間をこえると逆転するため、さらに
早く高真空に達すると思われる。
Measurement is performed in a small vacuum chamber to determine the amount of gas released (
(per unit surface area) was observed over time. This is shown in Figure 2. A is a CFRP board of a comparative example, and B is a CFRP board of an example.
It is an FRP board. All results were measured at room temperature. The example has a smaller amount of gas released than the comparative example,
It is thought that high vacuum will be reached more quickly. Next, B' is a case where a hot plate with a temperature of 80°C is placed in parallel at a position 20 cm away from the back surface of the FRP board of the example, and the temperature of the plate is about 73°C, which is higher than B' at the initial stage of degassing. Since gas release is active and reverses after 3 hours after degassing, it is thought that high vacuum will be reached even earlier.

(発明の効果) 実施例によって説明したように9本発明になるCFR,
Pミラーは、CFB、P基板の全表面に吸湿防止用の金
属被覆層があるので、運転休止中に吸湿することが少な
く、運転再開時に、すばやくチャンバー内を高真空にす
ることができるメリットがある。また裏面には黒色被覆
層をもうけているので、これと熱板あるいは冷却板を向
合せて配置することにより、CFRPミラーの温度をふ
く射によってコントロールできる。そして加熱すること
によりガス放出を促進し、早く運転状態にすることがで
き、また運転中の光照射によるミラーの温度上昇を、冷
却によって抑制できるメリットが6る。
(Effects of the Invention) As explained by the examples, the CFR of the present invention,
The P mirror has a metal coating layer on the entire surface of the CFB and P substrate to prevent moisture absorption, so it absorbs less moisture during suspension of operation, and has the advantage of quickly creating a high vacuum in the chamber when restarting operation. be. Furthermore, since a black coating layer is provided on the back surface, the temperature of the CFRP mirror can be controlled by radiation by arranging this and a heating plate or cooling plate facing each other. By heating, gas release can be promoted and the mirror can be brought into operation quickly, and the temperature increase of the mirror due to light irradiation during operation can be suppressed by cooling.

【図面の簡単な説明】[Brief explanation of drawings]

第1図は本発明のCFRPミラーの一例を示す縦断面図
および第2図は実施例、比較例のCFRPミラーモデル
の真空中脱°気時間とガス放出量の関係を示す図である
。 符号の説明 1・・・CF’RP基板   2・・・金属被覆層3・
・・接着剤       4・・・鏡面(アルミ蒸着層
)5・・・黒色被覆層
FIG. 1 is a longitudinal cross-sectional view showing an example of the CFRP mirror of the present invention, and FIG. 2 is a diagram showing the relationship between the degassing time in vacuum and the amount of gas released for the CFRP mirror models of Examples and Comparative Examples. Explanation of symbols 1... CF'RP board 2... Metal coating layer 3.
... Adhesive 4 ... Mirror surface (aluminum vapor deposited layer) 5 ... Black coating layer

Claims (1)

【特許請求の範囲】[Claims] 1、カーボン繊維強化プラスチック基板の全表面に金属
被覆層をもうけ、この表面の鏡面側にはアルミ蒸着層を
転写し、裏面には黒色被覆層をもうけてなるカーボン繊
維強化プラスチックミラー。
1. A carbon fiber reinforced plastic mirror made by forming a metal coating layer on the entire surface of a carbon fiber reinforced plastic substrate, transferring an aluminum vapor deposition layer to the mirror side of this surface, and forming a black coating layer on the back side.
JP21494584A 1984-10-12 1984-10-12 Carbon fiber reinforced plastic mirror Pending JPS6193404A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP21494584A JPS6193404A (en) 1984-10-12 1984-10-12 Carbon fiber reinforced plastic mirror

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP21494584A JPS6193404A (en) 1984-10-12 1984-10-12 Carbon fiber reinforced plastic mirror

Publications (1)

Publication Number Publication Date
JPS6193404A true JPS6193404A (en) 1986-05-12

Family

ID=16664166

Family Applications (1)

Application Number Title Priority Date Filing Date
JP21494584A Pending JPS6193404A (en) 1984-10-12 1984-10-12 Carbon fiber reinforced plastic mirror

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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0580212A (en) * 1991-09-24 1993-04-02 Mitsubishi Electric Corp Reflecting mirror made of fiber reinforced plastic
JPH05224295A (en) * 1992-02-17 1993-09-03 Mitsubishi Electric Corp Reflection mirror for screen projection type monitor
US20140170590A1 (en) * 2012-12-14 2014-06-19 Lynn Whalen Dual surface dental device for use in intraoral photography
WO2014140535A1 (en) * 2013-03-14 2014-09-18 University Of Surrey A carbon fibre reinforced plastic

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0580212A (en) * 1991-09-24 1993-04-02 Mitsubishi Electric Corp Reflecting mirror made of fiber reinforced plastic
JPH05224295A (en) * 1992-02-17 1993-09-03 Mitsubishi Electric Corp Reflection mirror for screen projection type monitor
US20140170590A1 (en) * 2012-12-14 2014-06-19 Lynn Whalen Dual surface dental device for use in intraoral photography
US9655503B2 (en) * 2012-12-14 2017-05-23 Lynn Whalen Dual surface dental device for use in intraoral photography
WO2014140535A1 (en) * 2013-03-14 2014-09-18 University Of Surrey A carbon fibre reinforced plastic
US10550232B2 (en) 2013-03-14 2020-02-04 University Of Surrey Thin film barrier coating for CFRP

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