1-16 of 16 Books
High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation
High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation
By Robert S. Jankovsky
Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure
Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure
By M. Moin Hussaini
Large-displacement structural durability analyses of simple bend specimen emulating rocket nozzle liners
Large-displacement structural durability analyses of simple bend specimen emulating rocket nozzle liners
By V. K. Arya
Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure
Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure
By Robert S. Jankovsky
RSRM nozzle fixed housing cooldown test final report
RSRM nozzle fixed housing cooldown test final report
By D. J. Bolieau
Development of thermal barriers for solid rocket motor nozzle joints
Development of thermal barriers for solid rocket motor nozzle joints
By Bruce M. Steinetz
Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle
Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle
By Kenneth J. Kacynski
Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20
Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20
By George T. Carson
Advanced small rocket chambers option 3
Advanced small rocket chambers option 3
By Donald M. Jassowski
A performance comparison of two small rocket nozzles
A performance comparison of two small rocket nozzles
By Lynn A. Arrington
Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle
Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle
By R. W. Marable
Comparison of response surface and kriging models in the multidisciplinary design of an aerospike nozzle
Comparison of response surface and kriging models in the multidisciplinary design of an aerospike nozzle
By Timothy W. Simpson
Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m(2) (350 psia)
Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m(2) (350 psia)
By Tamara A. Smith
A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center
A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center
By Kenneth J. Davidian
Shelf life extension for the lot AAE nozzle severance LSCs
Shelf life extension for the lot AAE nozzle severance LSCs
By M. Cook
Flight motor set 360L002 (STS-27R)
Flight motor set 360L002 (STS-27R)
By S. A. Meyer