Transient Computational Thermofluid-Dynamic Simulation of Hybrid Rocket Internal Ballistics-Reference-Cited by-同舟云学术

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Transient Computational Thermofluid-Dynamic Simulation of Hybrid Rocket Internal Ballistics

Published:2017-11 Issue:6 Volume:33 Page:1395-1409
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Di Martino G. D.¹,Carmicino C.¹,Savino R.¹

Affiliation:

1. University of Naples Federico II, 80125 Naples, Italy

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

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

Link

https://arc.aiaa.org/doi/pdf/10.2514/1.B36425

Reference48 articles.

1. Progress in Astronautics and Aeronautics;Altman D.,2007

2. OikineC. “New Perspectives for Hybrid Propulsion,” AIAA Paper 2006-4674, July 2006. doi:10.2514/6.2006-4674

3. Nammo hybrid rocket propulsion TRL improvement program

4. Optimal Design of Hybrid Rocket Motors for Microgravity Platform

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