Delta-Qualification of a 22N (5.0 lbf) MR-106B Monopropellant Hydrazine Thruster for the Mars Odyssey Spacecraft

Delta-Qualification of a 22N (5.0 lbf) MR-106B Monopropellant Hydrazine Thruster for the Mars Odyssey Spacecraft

Author(s):

Morgan,Olwen M. ( General Dynamics Space Propulsion Systems )
Fischer,Timothy L. ( Lockheed Martin Astronautics )
Guernsey,Carl S. ( Jet Propulsion Lab )

Publication title:

AIAA paper

Title of ser.:

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

Ser. no.:

2001

Pub. Year:

2001

No.:

2001-3632

Paper no.:

AIAA-2001-3632

Page(from):

1

Page(to):

9

Pages:

9

Pub. info.:

Reston, VA: American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050826
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference (JPC) & Exhibit
Conf. info. (Number):	37th
Conf. info. (Venue):	Salt Lake City, UT
Conf. info. (Date):	2001.07.08-2001.07.11
Note for article:	37th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit July 9-11, 2001/Salt Lake City, UT

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