HEAT PROTECTING MATERIAL

PURPOSE:To provide a heat protecting material for a space shuttle having a higher adiabatic property compared to conventional heat protecting materials. CONSTITUTION:An adiabatic structure is formed by laminating a plurality of combined sets of heat insulating boards 1-9 and reflecting boards 2-10....

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Bibliographische Detailangaben
Hauptverfasser:	KIRIHARA SEISHIN, KOJIMA YOSHIYUKI, HATTORI TOSHIO, YOSHINAKA TOSHISHIGE, MORINO MIKI, YAMAGUCHI SHIZUKA, WADA YUKIHIKO, IWAO KYOZO, KOBAYASHI TOMOYUKI, YOSHIOKA TAKATOSHI, YOSHIDA TAKEHIKO
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT AVIATION COSMONAUTICS PERFORMING OPERATIONS TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR
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