Experimental study on extendible and dual-bell nozzles under high altitude conditions

36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2000, Pages

  Kusaka, Kazuo ^a   Kumakawa, Akinaga ^b   Niino, Masayuki ^c   Konno, Akira ^c   Atsumi, Masahiro ^c  

^a KAKUDA RESEARCH CENTER   (Japan)

^b Natl Space Dev Agcy Japan   (Japan)

^c MITSUBISHI HEAVY INDUSTRIES LTD   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

BELLS; COMPUTATIONAL FLUID DYNAMICS; EXPANSION; HEAT TRANSFER PERFORMANCE; PARALLEL FLOW; PROPULSION;

AMBIENT PRESSURES; DUAL-BELL NOZZLES; FLOW REATTACHMENT; HEAT TRANSFER CHARACTERISTICS; NOZZLE EXPANSION RATIO; NOZZLE EXTENSION; RAPID TRANSITIONS; TRANSIENT PROCESS;

NOZZLES;

EID: 85088757446     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-3303     Document Type: Conference Paper

References (2)

1. Taniguchi H., Shibato Y.,"NASDA RLV Concept Study," Paper IAF-97-V.3.05, 1997.
2. Kuroda Y. et al., "Durability tests of subscale model of HOPE-X Plane QMS," NALTR-1294, 1994.