Computer Science
Scientific paper
Mar 1996
adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1996adspr..17...77k&link_type=abstract
Advances in Space Research, Volume 17, Issue 9, p. 77-80.
Computer Science
Scientific paper
For experimental testing of a Mars balloon probe in the upper layers of the Earth's atmosphere a specified parachute system was developed, fabricated and tested in 3 high-altitude balloon flights. The balloon volumes were 130000 and 180000 m^3 with the payloads of 500 - 900 kg; the maximum flight altitude reached 32 km. The experiments showed that one-canopy parachute system with the area of 1200 m^2 has certain advantages as compared to the four-canopy system and can be used both in Mars balloon tests in the Earth's stratosphere and as a parachute system of the descent apparatus for investigation of Mars.
Avrar J.
Kerzhanovich Viktor V.
Kotelnikov K. A.
Kotov B. B.
Kremnev Roald S.
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