NASA technical notes. D-65. Propellant vaporization as criterion for rocket-engine design, experimental effect of chamber diameter on liquid oxygen-heptane performance [with list of references]; by Marcus F. Heidmann.
Publication Title:
Propellant vaporization as criterion for rocket-engine design, experimental effect of chamber diameter on liquid oxygen-heptane performance [with list of references]; by Marcus F. Heidmann.
Display Title:
NASA technical notes. D-65. Propellant vaporization as criterion for rocket-engine design, experimental effect of chamber diameter on liquid oxygen-heptane performance [with list of references]; by Marcus F. Heidmann.
Series Title:
NASA technical notes.
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Heidmann, Marcus F.
Date:
Sept. 1959
Publish Date ISO Format:
1959-09-01T00:00:00Z
Publication Start:
19590901
Publication End:
19590930
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
4
Publication year:
1959
SuDoc number:
NAS 1.14:D-(nos.)
Description:
cover title, 22+ [4] p. il. 4°
Notes:
[Processed.]
Notes:
[Processed.] Φ For Sale by OTS, Commerce Dept. Paper, 75c.