Dual bell nozzles for rocket engines of launch vehicle upper stages and orbital transfer vehicles

Dual bell nozzles for rocket engines of launch vehicle upper stages and orbital transfer vehicles

Author(s):

Dumnov, G.E. ( Keldysh Research Center, Russia )
Ponomaryov, N.B.
Voinov, A.L.

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Ser. no.:

1997

Pub. Year:

1997

No.:

97-3089

Paper no.:

97-3089

Page(from):

1

Page(to):

7

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050849
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conf. info. (Number):	33rd
Conf. info. (Venue):	Seattle, WA
Conf. info. (Date):	1997.07.06-1997.07.09
Note for article:	33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, July 6-9, 1997/Seattle, WA

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