Theoretical performance of rocket engines using gaseous hydrogen in the ideal state at stagnation temperatures up to 200,000/sup 0/R
Technical Report
·
OSTI ID:5122947
None
- Research Organization:
- United Aircraft Corp., East Hartford, Conn. (USA)
- OSTI ID:
- 5122947
- Report Number(s):
- NP-16339
- Country of Publication:
- United States
- Language:
- English
Similar Records
THEORETICAL PERFORMANCE OF ROCKET ENGINES USING GASEOUS HYDROGEN IN THE IDEAL STATE AT STAGNATION TEMPERATURES UP TO 200,000 R. Report No. E-910093-30.
Thermodynamic properties and theoretical rocket performance of hydrogen to 100,000/sup 0/K and 1. 01325 X 10/sup 8/ N/m/sup 2/
COMPILATION OF THERMODYNAMIC PROPERTIES, TRANSPORT PROPERTIES, AND THEORETICAL ROCKET PERFORMANCE OF GASEOUS HYDROGEN
Technical Report
·
Fri Dec 31 23:00:00 EST 1965
·
OSTI ID:4467659
Thermodynamic properties and theoretical rocket performance of hydrogen to 100,000/sup 0/K and 1. 01325 X 10/sup 8/ N/m/sup 2/
Technical Report
·
Thu Dec 31 23:00:00 EST 1970
·
OSTI ID:5190242
COMPILATION OF THERMODYNAMIC PROPERTIES, TRANSPORT PROPERTIES, AND THEORETICAL ROCKET PERFORMANCE OF GASEOUS HYDROGEN
Technical Report
·
Thu Mar 31 23:00:00 EST 1960
·
OSTI ID:4186212