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Platform and launch initiation system for secondary spacecraft for launch vehicle
Platform and launch initiation system for secondary spacecraft for launch vehicle
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机译:运载火箭辅助航天器的平台和发射启动系统
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摘要
A platform and launch initiation control system for secondary spacecraft for a launch vehicle includes an aluminum honeycomb core sandwiched between top and bottom structural aluminum skins and strengthened by a spider-like stiffener. Spool inserts for engaging the secondary spacecraft are arranged on the platform. A computer processor based auxiliary payload support unit (APSU) is provided on the platform and receives power and enable signals through a single cable from the LV to permit the APSU to control the release of the secondary spacecraft transparently to the LV without impacting LV operations.
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