Decomposing solid micropropulsion nozzle performance issues

Ignition!

Advances in Chemical Propulsion

Les poudres, propergols et explosifs

Advanced chemical rocket propulsion

Solid propellant chemistry, combustion, and motor interior ballistics

Development of a quiet supersonic wind tunnel with a cryogenic adaptive nozzle

Results of tests performed on the acoustic quiet flow facility three-dimensional model tunnel

Development of quiet-flow supersonic wind tunnels for laminar-turbulent transition research

Aerodynamic design optimization via reduced Hessian SQP with solution refining

Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure

Supersonic laminar flow control research

Flight motor set 360L001 (STS-26R)

Nozzle thrust optimization while reducing jet noise

Effects of nozzle exit geometry and pressure ratio on plume shape for nozzles exhausting into quiescent air

The noise reduction potential of dual-stream coaxial rectangular improperly expanded jet flows

Dual-throat thruster thermal model

First NASA/Industry High Speed Research Program Nozzle Symposium

Experimental and computational investigation of a translating-throat, single-expansion-ramp nozzle