The report describes work concerning the design of a liquid Helium cooled infrared spectrometer for an Aerobee sounding rocket payload. The flight is designed to study the diffuse radiation from the Ecliptic and Galactic planes. The designs of the Dewar and electronics systems are not described here. The telescope will be an f3 7-inch aperture Cassegrain system. (Modified author abstract)
Infrared Spectrometer System for Aerobee Rocket Payload
1974
10 pages
Report
No indication
English
Aerobee 350 passes test with payload
NTRS | 1966
Aerobee 350 rocket instrumentation
NTRS | 1968
|Aerobee 350 Rocket Instrumentation
NTIS | 1968
|Development of aerobee 350 sounding rocket
Engineering Index Backfile | 1967
|DEVELOPMENT OF THE AEROBEE 350 SOUNDING ROCKET
AIAA | 1967
|