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
Link To Document :
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