Propellant vaporization as a criterion for rocket-engine design; Calculations of chamber length to vaporize various propellants / Richard J. Priem.
Vaporization rates were calculated for drops of n-heptane, ammonia, hydrazine, oxygen, and fluorine. The percent propellant vaporized is correlated with an effective chamber length for various spray conditions, and various engine-design and operating parameters. The results show that the effective c...
Saved in:
| Main Author: | |
|---|---|
| Corporate Author: | |
| Format: | Government Document Book |
| Language: | English |
| Published: |
Washington :
National Advisory Committee for Aeronautics,
[1958]
|
| Series: | Technical note (United States. National Advisory Committee for Aeronautics) ;
3883. |
| Subjects: |
PASCAL Offsite
| Call Number: |
Y 3.N 21/5:6/3883
|
|---|---|
| Y 3.N 21/5:6/3883 | Available Place a Hold |