Performance comparison of axisymmetric and three-dimensional hydrogen film coolant injection in a 110N hydrogen/oxyen rocket / Lynn A. Arrington and Brian D. Reed.

Author/creator Arrington, Lynn A.
Other author Reed, Brian D.
Other author Lewis Research Center.
Format Electronic
Publication Info[Cleveland, Ohio] : National Aeronautics and Space Administration, Lewis Research Center, [1992?]
Description1 online resource (20 p.) : digital, PDF file
Supplemental Contenthttps://purl.fdlp.gov/GPO/LPS125649

SeriesNASA technical memorandum ; 105967
NASA technical memorandum 105967. ^A467613
General noteTitle from title screen (viewed Aug. 25, 2010).
General noteGPO Cataloging Record Distribution Program (CRDP).
Bibliography noteIncludes bibliographical references (p. 8-9).
Issued in other formMicrofiche version: Arrington, Lynn A. Performance comparison of axisymmetric and three-dimensional hydrogen film coolant injection in a 110N hydrogen/oxyen rocket . 20 p.
GPO item number0830-D (online)
Govt. docs number NAS 1.15:105967
Stock numberN 93-16714 NASA

Availability

Library Location Call Number Status Item Actions
Electronic Resources Access Content Online ✔ Available