Experimental and Theoretical Investigation of Aerospike Nozzles in a Hybrid Rocket Propulsion System
47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition ; 2009 ; Orlando , Florida
01.01.2009
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Experimental and Theoretical Investigation of Aerospike Nozzles in a Hybrid Rocket Propulsion System
British Library Conference Proceedings | 2009
|Department highlights - Aerospike rocket nozzles take flight
Online Contents | 2004
Numerical investigation on linear aerospike nozzles
AIAA | 2001
|Experimental and numerical studies on aerospike nozzles
AIAA | 1999
|Liquid Rocket Propulsion: RS-68 and Linear Aerospike
NTRS | 1999
|