Abstract: 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.
Type:
Application
Filed:
November 25, 2013
Publication date:
May 15, 2014
Applicant:
HKM Enterprises Inc.
Inventors:
Philip Smith, James England, Michael Darmody, Jack Rubidoux
Abstract: 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.
Type:
Grant
Filed:
April 15, 2011
Date of Patent:
December 17, 2013
Assignee:
HKM Enterprises Inc.
Inventors:
Philip Smith, James England, Michael Darmody, Jack Rubidoux