NASA technical notes. D-258. Propellant vaporization as criterion rocket-engine design: Experimental effect of combustor length, throat Diameter, injection velocity, and pressure on rocket combustor efficiency [with list of references]; by Bruce J. Clark.
Publication Title:
Propellant vaporization as criterion rocket-engine design: Experimental effect of combustor length, throat Diameter, injection velocity, and pressure on rocket combustor efficiency [with list of references]; by Bruce J. Clark.
Display Title:
NASA technical notes. D-258. Propellant vaporization as criterion rocket-engine design: Experimental effect of combustor length, throat Diameter, injection velocity, and pressure on rocket combustor efficiency [with list of references]; by Bruce J. Clark.
Series Title:
NASA technical notes.
Corporate Agency Authors:
National Aeronautics and Space Administration
Sort Author:
National Aeronautics and Space Administration
Authors:
Clark, Bruce J.
Date:
Apr. 1960
Publish Date ISO Format:
1960-04-01T00:00:00Z
Publication Start:
19600401
Publication End:
19600430
Corporate/Agency Author:
National Aeronautics and Space Administration
Publication month:
9
Publication year:
1960
SuDoc number:
NAS 1.14:D-(nos.)
Description:
cover title, 27 p.+[2] leaves, il. 4°
Notes:
[Processed.]
Notes:
[Processed.] Φ For Sale by OTS, Commerce Dept. Paper, 75c.