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Comparison of theoretical and experimental thrust performance of a 1030:1 area ratio rocket nozzle at a chamber pressure of 2413 kN/m²(350 psia)

Author: Tamara A Smith; Albert J Pavli; Kacynski, Kenneth J.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
Publisher: [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va.] : [For sale by the National Technical Information Service], 1987.
Series: NASA technical paper, 2725.
Edition/Format:   Book   Microform : National government publication : Microfiche : EnglishView all editions and formats
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Material Type: Government publication, National government publication
Document Type: Book
All Authors / Contributors: Tamara A Smith; Albert J Pavli; Kacynski, Kenneth J.; United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.
OCLC Number: 22136931
Notes: Distributed to depository libraries in microfiche.
Reproduction Notes: Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1987. 1 microfiche.
Description: 1 volume.
Series Title: NASA technical paper, 2725.
Responsibility: Tamara A. Smith, Albert J. Pavli, and Kenneth J. Kacynski.

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