Results 161 to 170 of about 13,247 (287)

Conjugate Analysis of Rocket Nozzle Ablation [PDF]

open access: yes47th AIAA Thermophysics Conference, 2017
Peter G. Cross, Iain D. Boyd
openaire   +1 more source

Determination of the effects of nozzle nonlinearities upon nonlinear stability of liquid propellant rocket motors [PDF]

open access: yes
The research is reported concerning the development of a three-dimensional nonlinear nozzle admittance relation to be used as a boundary condition in the nonlinear combustion instability theories for liquid propellant rocket engines.
Padmanabhan, M. S.   +2 more
core   +1 more source

Effect of gaseous and solid simulated jet plumes on an 040A space shuttle launch configuration at m=1.6 to 2.2 [PDF]

open access: yes
The effect of plume-induced flow separation and aspiration effects due to operation of both orbiter and the solid rocket motors on a 0.019-scale model of the launch configuration of the Space Shuttle Vehicle is determined.
Blackwell, K. L.   +5 more
core   +1 more source

Development and demonstration of flueric sounding rocket motor ignition [PDF]

open access: yes
An analytical and experimental program is described which established a flueric rocket motor ignition system concept incorporating a pneumatic match with a simple hand pump as the only energy source.
Marchese, V. P.
core   +1 more source

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