Hybrid rocket engines: The benefits and prospects

Aerospace Science and Technology

Volumn 11, Issue 1, 2007, Pages 55-60

  Davydenko, N A ^a   Gollender, R G ^a   Gubertov, A M ^a   Mironov, V V ^a   Volkov, N N ^a  

^a KELDYSH RESEARCH CENTER   (Russian Federation)

Author keywords

Hybrid rocket engines; Oxidizer; Solid fuel

Indexed keywords

CURRENT VOLTAGE CHARACTERISTICS; HEAT RESISTANCE; MACHINE DESIGN;

HYBRID ROCKET ENGINES (HRE); ORBIT INSERTION; PAYLOADS; THERMAL PROTECTION;

ROCKET ENGINES;

EID: 33847224190     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ast.2006.08.008     Document Type: Article

References (1)

1. M.J. Chiaverini, K.K. Kuo, A. Peretz, G.C. Harting, Regression rate and heat transfer correlations for HTPB/GOX combustion in a hybrid rocket motor, AIAA Paper No 98-3185, 1998