FIELD: astronautics.
SUBSTANCE: group of inventions relates to the military equipment. In the first variant of the space head (SH), including the transition compartment for fixing the head fairing and the payload, on the inner surface of the transition compartment, the detachable parts of the separable boards of the electrical connectors and the on-board equipment are arranged by means of the attachment points. On the outer surface of the transfer compartment, at least an antenna device is installed and niches for undivided and separable electrical connectors are made. Non-separable electrical connectors are protected by an overhead fairing. On the edging of a niche with separable electrical connectors, a spring-loaded cover is hinged. In the second variant, the SH separable electrical connectors are located on the payload, opposite to which the hatch is made in the head fairing. Spring-loaded cover, covering the hatch, is fixed on the sash of the head fairing.
EFFECT: increased operational capabilities of the SH through efficient use of useful volume.
4 cl, 9 dwg
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SPACECRAFT HEAD SERVICING HATCH | 2012 |
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METHOD OF PAYLOAD INTEGRATION AND DEVICE TO THIS END | 2014 |
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SPACE HEAD FOR GROUP LAUNCH OF SATELLITES | 2010 |
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METHOD OF SPACESHIP SPACECRAFT NOSE CONE ASSEMBLY AND DEVICE TO THIS END | 2014 |
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Authors
Dates
2018-10-23—Published
2017-10-05—Filed