A payload system and a sounding rocket program are described. The payload was equipped with three experiments, and attitude control, and a land recovery system. The sounding rocket motor was a Skylark 6 type. Positioning, transmission to the ground, and recovery were the main technical functions of the system. Infrared radiation in the wave ranges 2.5 to 17 microns and 50 to 160 microns as well as 1.27 micron were measured in order to determine the influence of O, CO2, O3, NO, OH, and O2 emission on the energy balance in the altitude between 70 and 180 km.
Sounding Rocket Program Aeronomie. The Payload M-I in the Project MAP-Wine
1984
77 pages
Report
No indication
English
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