A Preliminary Model for Spacecraft Propulsion Performance Analysis based on Nuclear Gain and Subsystem Mass-Power Balances

A Preliminary Model for Spacecraft Propulsion Performance Analysis based on Nuclear Gain and Subsystem Mass-Power Balances

Author(s):

Chakrabarti, S. ( NASA Marshall Space Flight Center )
Schmidt, G.R.
Thio, Y.C.
Hurst, C.M.

Publication title:

AIAA paper

Title of ser.:

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

Ser. no.:

1999

Pub. Year:

1999

No.:

99-2838

Paper no.:

99-2838

Page(from):

1

Page(to):

11

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050872
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conf. info. (Number):	35th
Conf. info. (Venue):	Los Angeles, CA
Conf. info. (Date):	1999.06.20-1999.06.23
Note for article:	35th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit 20-24 June 1999 Los Angeles, California

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