NASA contractor report CR (series). 696. Theoretical performance of rocket engines using gaseous hydrogen in ideal state at stagnation temperatures up to 200,000 R [with list of references]; by R. Roback.
Publication Title:
Theoretical performance of rocket engines using gaseous hydrogen in ideal state at stagnation temperatures up to 200,000 R [with list of references]; by R. Roback.
Display Title:
NASA contractor report CR (series). 696. Theoretical performance of rocket engines using gaseous hydrogen in ideal state at stagnation temperatures up to 200,000 R [with list of references]; by R. Roback.
Series Title:
NASA contractor report CR (series).
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Roback, R.
Author place:
Washington, D.C.
Author zip:
20546
Date:
Feb. 1967
Publish Date ISO Format:
1967-02-01T00:00:00Z
Publication Start:
19670201
Publication End:
19670228
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
11
Publication year:
1967
SuDoc number:
NAS 1.26:(nos.)
Description:
cover title, vi+215 p. il. 4°
Notes:
[Prepared under contract NASw-847 by United Aircraft Corporation, East Hartford, Conn.]
Notes:
[Prepared under contract NASw-847 by United Aircraft Corporation, East Hartford, Conn.] Φ For Sale by OTS, Commerce Dept. Paper, $3.75.