Modeling and testing of a tube-in-tube separation mechanism of bodies in space

Author:

Michaels Dan,Gany Alon

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference16 articles.

1. Calculation and Design of Rocket Separation Systems;Kolesnikov,2006

2. D.H. Mitchell, Flight Separation Mechanisms, NASA Space Vehicle Design Criteria (Structures), NASA/SP-8056, Washington, DC, USA, 1970.

3. J. Stockinger, F. Shen, G. Bowers, M. Pan, I. Whalley, Delta IV evolved expendable launch vehicle ordnance overview, in: Proceedings of the 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, 2005

4. S.L. Mayers, B.B. Bernard, R.K. Smith, A. Patterson, ARES I stage separation system design certification testing, in: Proceedings of the56th JANNAF Propulsion Meeting, 2009.

5. K.K. Konno, D.A. Catalano, T.M. Krivanek., Evaluation of separation mechanism design for the Orion/Ares Launch Vehicle, in: Proceedings of the 35th Aerospace Mechanisms Symposium, (NASA report TM)-2008-215182, 2008.

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