Experimental evaluation of a subscale gaseous hydrogen/gaseous oxygen coaxial rocket injector
By: Timothy D. Smith ... [et al.].
Contributors: Smith, Timothy D.; NASA Glenn Research Center.
Series: NASA/TM -- 2002-211982; NASA technical memorandum -- 211982.
Publisher: National Aeronautics and Space Administration, Glenn Research Center; Available from NASA Center for AeroSpace Information
Published: 2002
Place of publication: Cleveland, Ohio; Hanover MD
Language: eng
Format: Microform
Subjects: Rocket engines.; Injectors.; Gaseous rocket propellants.; Rocket engine design.
Notes: Shipping list no.: 2003-0312-M.

"November 2002."

Also available via Internet from the NASA web site. Address as of 3/19/04: http://gltrs.grc.nasa.gov/reports/2002/TM-2002-211982.pdf; current access available via PURL.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2003]. 1 microfiche.