Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m(2) (350 psia)
By: Tamara A. Smith, Albert J. Pavli and Kenneth J. Kacynski.
Contributors: Kacynski, Kenneth J.; Pavli, Albert J.; Lewis Research Center
Publisher: Lewis Research Center
Published: 1987
Place of publication: Cleveland, Ohio
Number of pages: 21
Subjects: Nozzle design; Rocket nozzles
Notes: Bibliographical references: p.21.