1-14 of 14 Books
7.5K lbf thrust engine preliminary design for orbit transfer vehicle
7.5K lbf thrust engine preliminary design for orbit transfer vehicle
By Warren R. Hayden
Fiber-reinforced ceramic composites for Earth-to-orbit rocket engine turbines
Fiber-reinforced ceramic composites for Earth-to-orbit rocket engine turbines
By Jerry W. Brockmeyer
A comparison of analytical results for 20 K LOX/hydrogen instabilities
A comparison of analytical results for 20 K LOX/hydrogen instabilities
By Mark D. Klem
A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis
A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis
By Kenneth John Kacynski
Dual-throat thruster thermal model
Dual-throat thruster thermal model
By R. L. Ewen
Highly Evolved Expendable Launch Vehicle (HEELV) for the HRST program
Highly Evolved Expendable Launch Vehicle (HEELV) for the HRST program
By
A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis
A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis
By Kenneth J. Kacynski
A transient model of the RL10A-3-3A rocket engine
A transient model of the RL10A-3-3A rocket engine
By Michael P. Binder
The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios
The prediction of nozzle performance and heat transfer in hydrogen/oxygen rocket engines with transpiration cooling, film cooling, and high area ratios
By Kenneth John Kacynski
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
Predicted performance of an integrated modular engine system
Predicted performance of an integrated modular engine system
By Michael P. Binder
A unique high heat flux facility for testing hypersonic engine components
A unique high heat flux facility for testing hypersonic engine components
By Matthew E. Melis
Reduced H2-O2 mechanisms for use in reacting flow simulation
Reduced H2-O2 mechanisms for use in reacting flow simulation
By B. D. Hitch
Qualitative flow visualization of a 110-N hydrogen/oxygen laboratory model thruster
Qualitative flow visualization of a 110-N hydrogen/oxygen laboratory model thruster
By Wim A. de Groot