Burning Rate Comparison of a Mathematical Model with Experimental Results for AP/HTPB Based Composite Propellants
2018 AIAA Propulsion and Energy Forum, cincinnati, United States Of America, 9 - 11 July 2018, (Full Text)
- Publication Type: Conference Paper / Full Text
- Doi Number: 10.2514/6.2018-4578
- City: cincinnati
- Country: United States Of America
- Middle East Technical University Affiliated: Yes