发明授权
- 专利标题: Platform and launch initiation system for secondary spacecraft for launch vehicle
- 专利标题(中): 运载火箭二次航天器的平台和启动启动系统
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申请号: US13066471申请日: 2011-04-15
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公开(公告)号: US08608114B2公开(公告)日: 2013-12-17
- 发明人: Philip Smith , James England , Michael Darmody , Jack Rubidoux
- 申请人: Philip Smith , James England , Michael Darmody , Jack Rubidoux
- 申请人地址: US CO Denver
- 专利权人: HKM Enterprises Inc.
- 当前专利权人: HKM Enterprises Inc.
- 当前专利权人地址: US CO Denver
- 代理商 John L. Rogitz
- 主分类号: B64G1/00
- IPC分类号: B64G1/00 ; B64G1/22
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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