THERMODYNAMIC PROPERTIES OF ROCKET COMBUSTION PRODUCTS.
Quarterly technical rept. no. 3, 15 Apr-15 Jul 68,
PHILCO-FORD CORP NEWPORT BEACH CA AERONUTRONIC DIV
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The work described in this report is a continuing effort on the determination of the fragmentation pattern of LiF vapor which is in equilibrium with the condensed phase. Mass spectrometric technique involving beam modulation and gated detection was used. The experimental studies and some of the results obtained to date are discussed. Author
- Atomic and Molecular Physics and Spectroscopy
- Combustion and Ignition
- Rocket Engines