Title:
HIGH-PERFORMANCE PROPELLANT COMBINATION FOR ROCKET ENGINE
Document Type and Number:
Japanese Patent JPH02124791
Kind Code:
A
Abstract:
PURPOSE: To improve the storing time and a specific thrust of a rocket engine by combining oxidizing agents of [C3H5N3O]n and N2H5C(NO2)3, and a fuel such as B5H9, etc.
CONSTITUTION: The propellant is formed by combining [C3H5N3O]n or [C4H6N6 O]n or hydroxy terminal polybutadiene, an oxidizing agent, fuel and connectional additives. N2H5C(NO2)3 is used for the oxidizing agent. Further, B5H9 or B2H6 is used as the fuel.
Inventors:
HERUMAN FUEDE REIN SHIEIYAA
POORU AROISHIUSU OMERE GIISUBU
YOHANESU MARIA MURU
POORU AROISHIUSU OMERE GIISUBU
YOHANESU MARIA MURU
Application Number:
JP17786189A
Publication Date:
May 14, 1990
Filing Date:
July 10, 1989
Export Citation:
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