Published January 1952
| public
Journal Article
Quantitative evaluation of rocket propellants
- Creators
- Penner, S. S.
Chicago
An error occurred while generating the citation.
Abstract
A method for the quantitative evaluation of chemicals as rocket propellants is described. The procedure utilizes the fact that adiabatic expansion through a nozzle may be considered to be isentropic. Treatments are presented for two limiting conditions of expansion, corresponding to flow without chemical change and to flow which is characterized, at all times, by the existence of thermodynamic equilibrium.
Additional Information
Copyright © 1952 American Association of Physics Teachers. (Received July 9, 1951) Guggenheim Jet Propulsion Center Publication No. 12Additional details
- Eprint ID
- 14831
- Resolver ID
- CaltechAUTHORS:20090805-150338262
- Created
-
2009-08-13Created from EPrint's datestamp field
- Updated
-
2019-10-03Created from EPrint's last_modified field
- Caltech groups
- Guggenheim Jet Propulsion Center
- Other Numbering System Name
- Guggenheim Jet Propulsion Center Publication
- Other Numbering System Identifier
- 012