Explosive and thermic compositions or charges – Containing free boron or binary compounds of boron or boranes
Patent
1989-07-07
1990-08-21
Lechert, Jr., Stephen J.
Explosive and thermic compositions or charges
Containing free boron or binary compounds of boron or boranes
149 36, 149 42, 149 76, 149 88, C06B 4300
Patent
active
049503413
ABSTRACT:
A solid high-performance propellant for a rocket engine is described. The propellant is constituted by a combination of polyglycidylazide (GAP) ([C.sub.3 H.sub.5 N.sub.3 O].sub.n) or poly-3,3-bis(azidomethyl)oxetane (BAMO) ([C.sub.4 H.sub.6 N.sub.6 O].sub.n) with boron, aluminum, or aluminum hydride (AlH.sub.3) and a compound selected from the group consisting of hydrazinium nitroformate (N.sub.2 H.sub.5 C(NO.sub.2).sub.3), nitronium perchlorate (NO.sub.2 ClO.sub.4), or ammonium perchlorate (NH.sub.4 ClO.sub.4), together with other conventional additives.
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Korting Paul A. O. G.
Mul J. M.
Schoyer H. F. R.
European Space Agency
Lechert Jr. Stephen J.
Meller Michael N.
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