Multiple space vehicle launch system

Multiple space vehicle launch system

  • CN 105,775,164 A
  • Filed: 05/10/2013
  • Published: 07/20/2016
  • Est. Priority Date: 05/11/2012
  • Status: Active Application
First Claim
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1. Spacecraft Launch system (10) more than a kind, comprising:

  • First spacecraft (16), it includes the first core structure (36);

    Second spacecraft (18), it includes the second core structure (38) and is releasably attached to described first spacecraft (16) and relative to described first spacecraft (16) orientation, making when they are placed in trousers (14), the launch load from described first spacecraft (16) is sent to described second spacecraft (18) and is undertaken by described second spacecraft (18);

    WithIn wherein said first spacecraft (16) and the second spacecraft (18) one each comprised in electric propulsion unit (40) and chemistry and electric power hybrid propulsion unit (42), and described first core structure (36) is attached to described second core structure (38).

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