Abstract
The ultraviolet spectrum, atomic oxygen 130. 4nm radiation intensity, total plasma density, and electron temperature of a Mach 12 bow shock was obtained by a sounding rocket experiment launched from the Wallops Flight Facility on April 25, 1990, at 12:32 AM EST. A two-stage, Terrier Malamute rocket, which attained an apogee of 720 km, was used in this experiment. Optical data in the 200-400 nm wavelength range were obtained from 37 to 75 km at a vehicle velocity of 3. 5 km/sec. Electron probe and VUV OI 130. 4nm measurements were obtained near nose cone ejection at 37 km.
Original language | English (US) |
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State | Published - 1991 |
Externally published | Yes |
Event | AIAA 26th Thermophysics Conference, 1991 - Honolulu, United States Duration: Jun 24 1991 → Jun 26 1991 |
Other
Other | AIAA 26th Thermophysics Conference, 1991 |
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Country/Territory | United States |
City | Honolulu |
Period | 6/24/91 → 6/26/91 |
ASJC Scopus subject areas
- Mechanical Engineering
- Aerospace Engineering