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NEXT Performance Curve Analysis and ValidationPerformance curves of the NEXT thruster are highly important in determining the thruster's ability in performing towards mission-specific goals. New performance curves are proposed and examined here. The Evolutionary Mission Trajectory Generator (EMTG) is used to verify variations in mission solutions based on both available thruster curves and the new curves generated. Furthermore, variations in BOL and EOL curves are also examined. Mission design results shown here validate the use of EMTG and the new performance curves.
Document ID
20160009362
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Saripalli, Pratik
(Maryland Univ. College Park, MD, United States)
Cardiff, Eric
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Englander, Jacob
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Date Acquired
July 26, 2016
Publication Date
July 25, 2016
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
GSFC-E-DAA-TN33451
Report Number: GSFC-E-DAA-TN33451
Meeting Information
Meeting: AIAA/SAE/ASEE Joint Propulsion Conference
Location: Salt Lake City, UT
Country: United States
Start Date: July 25, 2016
End Date: July 27, 2016
Sponsors: American Inst. of Aeronautics and Astronautics, American Society for Electrical Engineers, Society of Automotive Engineers, Inc.
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
Electric
Thruster Performance
Propulsion
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