Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m(350 psia) /

by Smith, Tamara A.
Published 1987

Experimental thrust performance of a high-area-ratio rocket nozzle /

by Pavli, Albert J.
Published 1987

Experimental evaluation of heat transfer on a 1030:1 area ratio rocket nozzle /

by Kacynski, Kenneth J.
Published 1987

Nuclear thermal rocket nozzle testing and evaluation program /

by Davidian, Kenneth O.
Published 1993