Optics and Precision Engineering, Volume. 28, Issue 9, 1986(2020)
Design of pneumatic release device for sounding rocket payloads
References(4)
[2] [2] ITO T, YAMAMOTO T, NAKAMURA T, et al.. Sounding rocket SS-520 as a CubeSat launch vehicle ［J］.Acta Astronautica, 2020, 170: 206-223.
[3] [3] SLONGO L K, REIS J G, GAIKI D, et al.. Pre-flight qualification test procedure for nanosatellites using sounding rockets ［J］.Acta Astronautica, 2019, 159: 564-577.
[7] [7] GARCA F, NRMBERGE M R, TORRES R, et al.. ARION 1 reusable sounding rocket: the new microgravity platform in europe ［J］. Advances in Astronautics Science and Technology, 2018, 1(1): 23-30.
[8] [8] GIOVANNI ROSANOVA. NASA sounding rockets annual report 2018 ［R］. NASA Sounding Rockets Program Office, 2018.
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MA Xin, GAO Dong, BIAN Chun-jiang. Design of pneumatic release device for sounding rocket payloads[J]. Optics and Precision Engineering, 2020, 28(9): 1986
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Received: Feb. 25, 2020
Accepted: --
Published Online: Dec. 28, 2020
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