Diameter and position effect determination of diaphragm on hybrid rocket motor

Author:

Sun Xingliang,Tian Hui,Cai Guobiao

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference35 articles.

1. Optimal design of hybrid rocket motor powered vehicle for suborbital flight;Cai;Aerosp. Sci. Technol.,2013

2. Design and optimization of variable thrust hybrid rocket motors for sounding rockets;Rao;Sci. China Technol. Sci.,2012

3. Optimal design of hybrid rocket motors for microgravity platform;Casalino;J. Propuls. Power,2008

4. J. Dyer, E. Doran, Z. Dunn, et al., Design and Development of a 100Km Nitrous Oxide/Paraffin Hybrid Rocket Vehicle, 2007-5362, 2007.

5. R.K. K, A. Kuznetsov, Benveniste Design of a Lab-Scale Hydrogen Peroxide/Hydroxyl Terminated Polybutadiene Hybrid Rocket Motor, AIAA Paper 2003-4744, 2003 .

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