Study to determine feasibility of developing rocketsonde system for routine meteorological use; possible system would be single stage solid propellant rocket carrying instrumentation to desired altitude, at which point instrument container could be separated for descent by parachute; two tracking systems could provide necessary slant range information: radar and AN/GMD-2 Rawinsonde system; temperature measurements and temperature-sensing elements.
Low-cost meteorological rocket systems
Astronautics
Astronautics ; 3 , n 10
1958
Article (Journal)
English
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