Reduced temperature sensitivity launch motor
USH795H · kind H · statutory invention registration
2Cited by
0References
3Claims
0Family size
Assignee
Inventors
Key dates
| Filing date | — |
| Grant date | Jul 3, 1990 |
| Priority date | — |
| Expiry date | — |
Classification
- Technology area (CPC —)General
Abstract
A rocket motor that has a main exhaust nozzle area and a secondary exhaust ozzle area with the secondary exhaust nozzle area being closed by burst discs that rupture and open secondary nozzle areas when predetermined temperatures and pressures are reached when propellant is burned inside the rocket motor.
Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.