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Title:
HIGH-PERFORMANCE PROPELLANT COMBINATION FOR ROCKET ENGINE
Document Type and Number:
Japanese Patent JPH02124790
Kind Code:
A
Abstract:

PURPOSE: To improve the storing time and a specific thrust of a rocket engine by combing [C3H5N3O]n, Al, N2H5C(NO2)3, NH4ClO4, etc.

CONSTITUTION: The propellant is formed by combining [C3H5N3O]n or [C4H6N6 O]n, a fuel, an oxidizing agent and connectional additives. B, Al and Al hydride are used for the fuel. Further, a comd., which is selected from among N2H5C (NO2)3, NO2ClO4 and NH4ClO4, is used as the oxidizing agent.


Inventors:
HERUMAN FUEDE REIN SHIEIYAA
POORU AROISHIUSU OMERE GIISUBU
YOHANESU MARIA MURU
Application Number:
JP17786089A
Publication Date:
May 14, 1990
Filing Date:
July 10, 1989
Export Citation:
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Assignee:
YUUROPEAN SUPEESU AGENCY
International Classes:
B64G1/00; C06B33/08; C06B43/00; C06B45/10; C06B47/10; C06D5/00; F02K9/42; (IPC1-7): B64G1/00; C06D5/00; F02K9/42
Attorney, Agent or Firm:
Mitsuo Matsui