NASA technical notes. D-129. Combined effect of contraction ratio and chamber pressure on performance of gnseous-hydrogen-liquld-oxygen combustor for given propellant weight flow and oxidant-fuel ratio [with list of references]; by Martin Hersch.
Publication Title:
Combined effect of contraction ratio and chamber pressure on performance of gnseous-hydrogen-liquld-oxygen combustor for given propellant weight flow and oxidant-fuel ratio [with list of references]; by Martin Hersch.
Display Title:
NASA technical notes. D-129. Combined effect of contraction ratio and chamber pressure on performance of gnseous-hydrogen-liquld-oxygen combustor for given propellant weight flow and oxidant-fuel ratio [with list of references]; by Martin Hersch.
Series Title:
NASA technical notes.
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Hersch, Martin
Date:
Feb. 1961
Publish Date ISO Format:
1961-02-01T00:00:00Z
Publication Start:
19610201
Publication End:
19610228
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
11
Publication year:
1961
SuDoc number:
NAS 1.14:D-(nos.)
Description:
cover title, 13+ [4] p. il. 4°
Notes:
[Processed.]
Notes:
[Processed.] Φ For Sale by OTS, Commerce Dept. Paper, 50c.