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Accession Number:
AD0265025
Title:
PRESSURE AND TEMPERATURE IN THE EXHAUST OF SIDEWINDER MK 31 MOD O ROCKET MOTOR
Corporate Author:
NAVAL WEAPONS LAB DAHLGREN VA
Report Date:
1961-10-19
Abstract:
Temperature and pressure measurements were made in the exhaust stream of 15 statically fired Sidewinder Mk 31 Mod 0 rocket motors. The peak rise in temperature and pressure is presented in the form of contour plots extending to a distance of 90 ft downstream in the case of temperature and of 35 ft downstream for pressure. Author
Pages:
0001
File Size:
0.00MB
