Arcjet load characteristics
By: John A. Hamley ; prepared for the 21st International Electric Propulsion Conference cosponsored by the AIAA, DGLR, and JSASS, Orlando, Florida, July 18-20, 1990.
Contributors: United States. National Aeronautics and Space Administration.
Series: NASA technical memorandum -- 103190.
Publisher: NASA; For sale by the National Technical Information Service
Published: 1990
Place of publication: [Washington, D.C.]; [Springfield, Va
Language: eng
Format: Microform
Number of pages: 16
Subjects: Arc-jet rocket engines.; Arc jet engines.; Decomposition.; Flow velocity.; Hydrazines.; Loads (Forces)
Notes: Cover title.

Shipping list no.: 90-1086-M.

"AIAA-90-2579."

"E-5578"--Technical rept. documentation p.

Includes bibliographical references (p. 7-8).

Also available via Internet from the NASA Technical Report Server web site. Address as of 4/28/05: http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19900015865%5F1990015865.pdf; current access available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1990]. 1 microfiche : negative.

506-42-31.