Gas-generating agent for use in ducted rocket engine
First Claim
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1. A gas-generating agent for use in a ducted rocket engine, essentially consisting of one member selected from the group consisting of aliphatic polyethers represented by the formula:
- ##STR5## wherein n is in the range of 10 to 50 and m +l in the range of 1 to 10, and the general formula;
##STR6## wherein p, q, r, and z are each not less than 1 and p +q +r +z is in the range of 10 to 50, and a curing agent.
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Abstract
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.
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Citations
7 Claims
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1. A gas-generating agent for use in a ducted rocket engine, essentially consisting of one member selected from the group consisting of aliphatic polyethers represented by the formula:
- ##STR5## wherein n is in the range of 10 to 50 and m +l in the range of 1 to 10, and the general formula;
##STR6## wherein p, q, r, and z are each not less than 1 and p +q +r +z is in the range of 10 to 50, and a curing agent. - View Dependent Claims (2, 3, 4, 5, 6, 7)
- ##STR5## wherein n is in the range of 10 to 50 and m +l in the range of 1 to 10, and the general formula;
Specification