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Development Test of Spacecraft Separation Dynamics under Ground Conditions Автори: Gontarovsky V. Development Test of Spacecraft Separation Dynamics under Ground Conditions Автори: Gontarovsky V. Development Test of Spacecraft Separation Dynamics under Ground Conditions Автори: Gontarovsky V. Development Test of Spacecraft Separation Dynamics under Ground Conditions Автори: Gontarovsky V.
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17. Development Test of Spacecraft Separation Dynamics under Ground Conditions

Organization:

Yangel Yuzhnoye State Design Office, Dnipro, Ukraine

Page: Kosm. teh. Raket. vooruž. 2017 (2); 90-101

Language: Russian

Annotation: The paper describes the spacecraft separation system ground functional tests, including SC separation dynamics refinement, in the process of which the separation system operability is confirmed and the parameters characterizing separation dynamics are determined.

Key words:

Bibliography:
1. Kobelev V. N., Milovanov A. G. Spacecraft Injection Means. М., 2009. 528 p.
2. Fundamentals of Spacecraft Launch Vehicle Designing / Under the editorship of V. P. Mishin. М., 1991. 415 p.
3. Shenk H. Theory of Engineering Experiment. М., 1972. 376 p.
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17.2.2017 Development Test of Spacecraft Separation Dynamics under Ground Conditions
17.2.2017 Development Test of Spacecraft Separation Dynamics under Ground Conditions
17.2.2017 Development Test of Spacecraft Separation Dynamics under Ground Conditions
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