A novel kind of solid rocket propellant

Aerospace Science and Technology

Volumn 2, Issue 6, 1998, Pages 359-367

  Lo, Roger E ^a  

^a TECHNISCHE UNIVERSITÄT BERLIN   (Germany)

Author keywords

Cryogenic solids; High energy density matter; Hybrid propellants; Rocket propulsion; Solid propellants

Indexed keywords

EID: 0032350317     PISSN: 12709638     EISSN: None     Source Type: Journal    
DOI: 10.1016/S1270-9638(99)80024-8     Document Type: Article

References (6)

1. DeRose M., Pfeil K., Carrick P., Larson C., Tube Burner Studies of Cryogenic Solid Combustion, Phillipps Lab, Edwards AFB, AIAA-97-3076
2. Lo R.E., Technical Feasibility of Chemical Propulsion Systems with very high Performance, Proceedings of the XVIIIth Astronautical Congress, Belgrade, 25-29.9.1967, pp. 121-132
3. Lo R.E., Modulare Feststoffraketentreibsätze (Modular Rocket Propellant Grains), German Patent Application No. 197 56 794.0, Dec. 19, 1997
4. 3/Hydrocarbon), DLR/USAF; Report BMBW-FB W 7047, August 1970 (in German)
5. Voslamber B., Parametrische Analyse eines Ultra-hochdruck-Kryofeststofftriebwerks (Parametric Analysis of a Cryo Solid Motor With Ultrahigh Chamber Pressure), diploma thesis in rocket technology, Aerospace Institute, Berlin University of Technology, Oct. 1994 (in German)
6. Voslamber B., Voslamber M. and Lo R.E., Machbarkeitsstudie kryogene Feststoffbooster (Feasibility Study of Cryogenic Solid Boosters), German Space Agency DARA, Project 50TT 9631, Final report 2/1997 (in German)