Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m℗ø(350 psia)
By: Tamara A. Smith, Albert J. Pavli, and Kenneth J. Kacynski.
Contributors: Pavli, Albert J.; Kacynski, Kenneth J.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Series: NASA technical paper -- 2725.
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Office; For sale by the National Technical Information Service]
Published: 1987
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Subjects: Rocket engines.; Rockets (Aeronautics) -- Nozzles.
Notes: Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1987. 1 microfiche.