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Explore Books on
rocket nozzles

1-16 of 16 Books

View High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation By Robert S. Jankovsky

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

View Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure By M. Moin Hussaini

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

View Large-displacement structural durability analyses of simple bend specimen emulating rocket nozzle liners By V. K. Arya

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

View Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure By Robert S. Jankovsky

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

View RSRM nozzle fixed housing cooldown test final report By D. J. Bolieau

RSRM nozzle fixed housing cooldown test final report

RSRM nozzle fixed housing cooldown test final report

By D. J. Bolieau

View Development of thermal barriers for solid rocket motor nozzle joints By Bruce M. Steinetz

Development of thermal barriers for solid rocket motor nozzle joints

Development of thermal barriers for solid rocket motor nozzle joints

By Bruce M. Steinetz

View Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle By Kenneth J. Kacynski

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

View Aeropropulsive characteristics of isolated combined turbojet/ramjet nozzles at Mach numbers from 0 to 1.20 By George T. Carson

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

View Advanced small rocket chambers option 3 By Donald M. Jassowski

Advanced small rocket chambers option 3

Advanced small rocket chambers option 3

By Donald M. Jassowski

View A performance comparison of two small rocket nozzles By Lynn A. Arrington

A performance comparison of two small rocket nozzles

A performance comparison of two small rocket nozzles

By Lynn A. Arrington

View Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle By R. W. Marable

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

View Comparison of response surface and kriging models in the multidisciplinary design of an aerospike nozzle By Timothy W. Simpson

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

View 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

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

View A detailed description of the uncertainty analysis for high area ratio rocket nozzle tests at the NASA Lewis Research Center By Kenneth J. Davidian

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

View Shelf life extension for the lot AAE nozzle severance LSCs By M. Cook

Shelf life extension for the lot AAE nozzle severance LSCs

Shelf life extension for the lot AAE nozzle severance LSCs

By M. Cook

View Flight motor set 360L002 (STS-27R) By S. A. Meyer

Flight motor set 360L002 (STS-27R)

Flight motor set 360L002 (STS-27R)

By S. A. Meyer