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The Star is a family of US solid-propellant rocket motors originally developed by Thiokol and used by many space propulsion and launch vehicle stages. They are used almost exclusively as an upper stage, often as an apogee kick motor.
References
- ↑ "Space debris mitigation: the case for a code of conduct". ESA. European Space Agency. 15 April 2005. Retrieved 14 November 2014.
- ↑ Juno II Summary Project Report, Volume II (PDF) (Technical report). NASA. 1962. D-608.
- ↑ Scott R. Starin and John Eterno (January 2011). "Attitude Determination and Control Systems" (PDF). NASA.
- ↑ "General Description of Sounding Rockets". Johns Hopkins.
- ↑ Dawn Journal, 12 September 2007
- ↑ US 3030049,Pilkington Jr., William C.; McDonald, William S.& Wells, Willard H.,"Satellite spin control",published 1962-04-17, assigned to Secretary of the United States Army
- ↑ Ishii, Nobuaki (March 2005). "Separation motion analysis of sounding rockets using unbalanced YoYo mechanism". ISAS proceedings of 14th Workshop on Astrodynamics and Flight Mechanics 2004: A Collection of Technical Papers: 105–109. ISSN 0918-8053. S2CID 125586338.
In sounding rocket experiments and a final stage of satellite insertion, when the payload section or the satellite is separated from the lower motor, collision of the motor due to the residual thrust should be avoided. Conventionally, a tumble motor (small solid rocket propellant) or Yo tumbler is utilized for the collision avoidance.
- ↑ Krebs, Gunter Dirk. "Ohsumi". Gunter's Space Page. Retrieved 2024-06-28.
- ↑ "Space station crew has close call with space junk". USA Today. March 12, 2009. Archived from the original on March 25, 2009.