Burning Rate Comparison of a Mathematical Model with Experimental Results for AP/HTPB Based Composite Propellants

Özcan S., cürdaneli s., ULAŞ A.

2018 AIAA Propulsion and Energy Forum, cincinnati, United States Of America, 9 - 11 July 2018

  • Publication Type: Conference Paper / Full Text
  • Doi Number: 10.2514/6.2018-4578
  • City: cincinnati
  • Country: United States Of America