CPC B64G 1/645 (2013.01) | 2 Claims |
1. A satellite deployment impact driver separation system, comprising:
a first payload side element;
a second launch vehicle side element;
a first payload side bolt or nut;
a second launch vehicle side nut or bolt; and
a dedicated collocated impact actuator,
wherein said first payload side element and said second launch vehicle side element are joined by said first payload side bolt or nut and said second launch vehicle side nut or bolt respectively,
wherein said dedicated collocated impact actuator dedicatedly connects to said first payload side bolt or nut or said second launch vehicle side nut or bolt respectively,
said dedicated collocated impact actuator permits removal of said first payload side bolt or nut from said second launch vehicle side nut or bolt respectively for separation of said first payload side element and said launch vehicle side second element.
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