DocumentCode
3515631
Title
Advanced Chemical Propulsion for Science Missions
Author
Liou, Larry
Author_Institution
NASA John H. Glenn Res. Center, Cleveland, OH
fYear
2008
fDate
1-8 March 2008
Firstpage
1
Lastpage
10
Abstract
The advanced chemical propulsion technology area of NASA´s in-space technology project is investing in systems and components for increased performance and reduced cost of chemical propulsion technologies applicable to near-term science missions. Presently the primary investment in the advanced chemical propulsion technology area is in the AMBR high temperature storable bipropellant rocket engine. Scheduled to be available for flight development starting in year 2008, AMBR engine shows a 60 kg payload gain in an analysis for the Titan-Enceladus orbiter mission and a 33% manufacturing cost reduction over its baseline, state-of-the-art counterpart. Other technologies invested include the reliable lightweight tanks for propellant and the precision propellant management and mixture ratio control. Both technologies show significant mission benefit, can be applied to any liquid propulsion system, and upon completion of the efforts described in this paper, are at least in parts ready for flight infusion. Details of the technologies are discussed.
Keywords
aerospace propulsion; rocket engines; AMBR high temperature storable bipropellant rocket engine; Titan-Enceladus orbiter mission; advanced chemical propulsion; liquid propulsion system; mixture ratio control; precision propellant management; science missions; Chemical technology; Costs; Engines; Investments; Job shop scheduling; Manufacturing; Payloads; Propulsion; Rockets; Temperature;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Conference, 2008 IEEE
Conference_Location
Big Sky, MT
ISSN
1095-323X
Print_ISBN
978-1-4244-1487-1
Electronic_ISBN
1095-323X
Type
conf
DOI
10.1109/AERO.2008.4526549
Filename
4526549
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