Oblon, Spivak, McClelland, Maier & Neustadt
Gas-generating agent for use in ducted rocket engine
 A gas-generating agent for use in a ducted rocket engine essentially consists of an aliphatic polyester represented by the formula: ##STR1## or the formula: ##STR2## and a curing agent and optionally incorporating therein additives such as a curing catalyst. 
Japan as represented by Director General, Technical Research and Development Institute, Japan Defense Agency Nippon Oil & Fats Co., Ltd.
C C C C C
C06D C06B C08G C08G C08G
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Tadashi Goro Naminosuke Haruaki
Sonobe Nakashita Kubota Shimizu