THE NUCLEAR RAMJET PROPULSION SYSTEM
The most practical nuclear ramjet systems consist of a suituble inlet diffusor system followed by a singlepass, straight-through heat exchanger (reactor) which couples into a typical exhaust nozzle. Within this framework, possibilities ars governed by the aerodynamic requirements of flight, the nuclear requirements of the reactor, the chemical problems associated with breathing air, and the mechanical properties of materials at elevated temperatures. The major research and development areas which must be entered in the actual production of such an engine are discussed. (W.D.M.)
- Research Organization:
- California. Univ., Livermore. Lawrence Radiation Lab.
- DOE Contract Number:
- W-7405-ENG-48
- NSA Number:
- NSA-14-001143
- OSTI ID:
- 4217328
- Report Number(s):
- UCRL-5625
- Resource Relation:
- Other Information: Orig. Receipt Date: 31-DEC-60
- Country of Publication:
- United States
- Language:
- English
Similar Records
Experimental investigation of the ignition and flammability limits of various hydrocarbon fuels in a two-dimensional solid-fuel ramjet. Master's thesis
THE NUCLEAR RAMJET PROPULSION SYSTEM
Numerical prediction of low frequency combustion instability in a model ramjet combustor
Technical Report
·
Mon Jun 01 00:00:00 EDT 1987
·
OSTI ID:4217328
THE NUCLEAR RAMJET PROPULSION SYSTEM
Technical Report
·
Mon May 15 00:00:00 EDT 1961
·
OSTI ID:4217328
Numerical prediction of low frequency combustion instability in a model ramjet combustor
Conference
·
Tue Dec 31 00:00:00 EST 1996
·
OSTI ID:4217328
+1 more