Development of advanced technologies for future cryogenic thrust chamber applications

33rd Joint Propulsion Conference and Exhibit

Volumn , Issue , 1997, Pages 1-11

  Zinner, W ^a   Haeseler, D ^a   Mading C ^a   Rubinskij, V ^b   Gorochov, V ^b   Hrisanfov, S ^b   Nikulin, G ^c  

^a AIRBUS GROUP INNOVATIONS   (Germany)

^b Chemiautomatics Design Bureau (CADB)   (Russian Federation)

^c KELDYSH RESEARCH CENTER   (Russian Federation)

Author keywords

[No Author keywords available]

Indexed keywords

BELLS; COMBUSTION CHAMBERS; CRYOGENICS; DESIGN; NOZZLE DESIGN; NOZZLES; PROPULSION; ROCKET ENGINES; ROCKET NOZZLES; ROCKETS;

ADVANCED TECHNOLOGY; DUAL-BELL NOZZLES; ENGINE APPLICATION; EXPECTED IMPROVEMENTS; PERFORMANCE ENHANCING; SPACE INFRASTRUCTURES; TECHNOLOGY DEVELOPMENT; TRANSPIRATION COOLING;

SOFTWARE TESTING;

EID: 84962860301     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (8)

1. V.R. Roubsinsky, V.D. Gorokchov, V.A. Orlov, V.I. Kholodny, CADB; W. Zinner, Dasa Combustion ChamberTranspiration Cooling 5th Propulsion in Space Transportation Paris, 22-24 May, 1996
2. M. Popp- G. Schmidt, Dasa Advanced Thrust Chambers 5th Propulsion in Space Transportation Paris, 22-24 May, 1996
3. H. Immich, Dasa-M. Caporicci, ESA FESTIP Technology Development in Liquid Rocket Propulsion for Reusable Launch Vehicles AIAA-96-3113
4. R.J. Quentmeyer Rocket Combustion Chamber Life Enhancing Design Concepts AIAA-90-2116
5. Prof. Dr. S. Fischer Untersuchung spezieller Probleme der Transpirationskuhlung von Raketenbrennkammerwanden TU-Dresden, 1997
6. J.C.Y Koh-J.L Dutton, B.A. Benson Fundamental Study of Transpiration Cooling NASA CR-134523, 1973
7. T.V. Nguyen, J.L. Pieper, GenCorp Aerojet Nozzle Flow Separation 5th Propulsion in Space Transportation Paris, 22-24 May, 1996
8. M. Horn S. Fisher Dual-Bell Altitude Compensating Nozzles Rocketdyne Division