Thrust

Thrust chamber performance using Navier-Stokes solution: final report

prepared for National Aeronautics and Space Administration, Marshall Space Flight Center by John S. Chan, Jon A. Freeman

Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability

Mary L. Mason and James R. Burley II.

A simple dynamic engine model for use in a real-time aircraft simulation with thrust vectoring

Steven A. Johnson.

A first scramjet study

George Emmanuel.

High-speed engine/component performance assessment using exergy and thrust-based methods

D.W. Riggins.

Optimal pitch thrust-vector angle and benefits for all flight regimes

Glenn B. Gilyard, Alexander Bolonkin.

High pressure, earth storable rocket technology

D.M. Jassowski.

The PIT MkV pulsed inductive thruster

C. Lee Dailey and Ralph H. Lovberg.

Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure

Robert S. Jankowsky, John M. Kazaroff, Albert J. Pavli.

Static thrust-vectoring performance of nonaxisymmetric convergent-divergent nozzles with post-exit yaw vanes

Robert J. Foley, Odis C. Pendergraft, Jr.