AUTOPYROLYSABLE COMPOSITION FOR AEROBE PROPULSION THE OXIDIZER OF WHICH IS AN EXPLOSIVE
Assignee
SOCIETE NATIONALE DES POUDRES ET EXPLOSIFS
Filed
Jul 29, 1980
Granted
Feb 4, 1992
Location
PARIS FR
Abstract
An autopyrolyzable solid composition for aerobic propulsion consists essentially of an oxidizing agent, a binder and a crosslinking agent. The oxidizing agent is a nitrated explosive material wherein the amount, by weight, of oxygen atoms fixed to the nitrogen atoms of the nitrate groups exceeds 40 percent relative to the total weight of the molecule. The binder is a polyalkadiene having functional terminal groups, such as --OH or --COOH groups, reactive with the crosslinking agent which can have isocyanate, epoxy or aziridinyl functions.
Source: Google Patents
35 USC §181 Secrecy Order
Imposed
Apr 6, 1982
Rescinded
May 11, 1990
Duration
8 years, 1 month
Inventor
- 1JEAN-DANIEL M. BERARD
Record Details
- Patent number
- US 5085717
- Application
- 06178541
- Aerospace match
- Yes
- Dataset source
- 35 USC §181 SO records
Browse by Assignee
SOCIETE NATIONALE DES POUDRES ET EXPLOSIFSMore from this assignee
Related by domain
GAS TURBINE ENGINE COMBUSTOR HAVING TRAPPED DUAL VORTEX CAVITY
General Electric
SOLID ROCKET PROPELLANT
GAS TURBINE ENGINE FAN (U)
General Electric
TURNING VANE ARRANGEMENT FOR IR SUPPRESSORS
SIKORSKY AIRCRAFT CORPORATION
MODULAR ROCKET BOOSTED PENETRATING WARHEAD
LOCKHEED MARTIN CORP.
INTEGRAL SOLID BOOSTER AND HYBRID THRUST SUSTAINING SYSTEM AND PROJECTILE INCORPORATING THE SAME
ENVIRONMENTAL AEROSCIENCE CORPORATION