Numerical and Experimental Investigation of Unidirectional Vortex Injection in Hybrid Rocket Engines-Reference-Cited by-同舟云学术

Numerical and Experimental Investigation of Unidirectional Vortex Injection in Hybrid Rocket Engines

Published:2013-09 Issue:5 Volume:29 Page:1097-1113
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Bellomo N.¹,Barato F.¹,Faenza M.¹,Lazzarin M.¹,Bettella A.¹,Pavarin D.¹

Affiliation:

1. Department of Mechanical Engineering, University of Padua, 35131 Padova, Italy

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.B34506

Reference14 articles.

1. Solid-Fuel Regression Rate Behavior of Vortex Hybrid Rocket Engines

2. KnuthW. H.BemowskiP. A.GramerD. J.MajdalaniJ.RothbauerW. J. “Gas-Fed, Vortex Injection Hybrid Rocket Engine,” SBIR Phase I Final Technical Rept. NASA/Marshall Space Flight Center, NASA/MSFC Contract No. NAS8-40679, Huntsville, AL, 1996.

3. KnuthW. H.ChiaveriniM. J.GramerD. J.SauerJ. A. “Final Report on Gas-Fed, Vortex Injection Hybrid Rocket Engine,” Phase II SBIR Project, Orbital Technological Corp., NASA Contract No. NAS8-97015, Rept. OTC-GS055-FR-99-1, 1999.

4. Development of a small sounding hybrid rocket with a swirling-oxidizer-type engine

5. Progress in Astronautics and Aeronautics;Chiaverini M. J.,2007

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