TY - GEN
T1 - Review of chemical-electric multimode space propulsion
AU - Rovey, Joshua L.
AU - Lyne, Christopher T.
AU - Mundahl, Alex J.
AU - Rasmont, Nicolas
AU - Glascock, Matthew S.
AU - Wainwright, Mitchell J.
AU - Berg, Steven P.
N1 - Funding Information:
Support for this work was provided through the NASA Marshall Space Flight Center, NASA grant NNM15AA09A, and the Air Force University Nano-satellite Program through the Utah State University Research Foundation, grant CP0039814. Additional support was provided by NASA Goddard Space Flight Center through the NASA Undergraduate Student Instrument Project grant NNX16AI85A, and the University of Missouri System Fast Track Program, FastTrack-16003R. M. Wainwright thanks the Department of Education for their Graduate Assistance in Areas of National Need Fellowship P200A150309. M. S. Glascock would like to graciously thank the NASA Space Technology Research Fellowship program for funding his graduate research via grant NNX15AP31H.
Publisher Copyright:
© 2019, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2019
Y1 - 2019
N2 - Multimode propulsion is the integration of two or more propulsive modes into a single spacecraft propulsion system. In a multimode propulsion system, the key attribute is shared propellant between the different propulsive modes. Multimode propulsion is emerging as an enabling technology that promises enhanced capabilities for spacecraft and space missions, and can therefore play an important role in the future of in-space propulsion. Specifically, multimode propulsion has potential to provide unprecedented flexibility and adaptability to spacecraft, as well as provide mass savings for certain missions. These benefits extend to both medium and large spacecraft, as well as small satellites. Numerous multimode concepts have been explored and documented in the literature. Concepts combining cold gas, monopropellant, bipropellant, and solid chemical propulsion with electrothermal, electrostatic, and electromagnetic electric propulsion have all been investigated. Electrospray electric propulsion paired with monopropellant chemical propulsion has perhaps received the most recent attention. We review the concept of multimode propulsion, mission analyses, benefits, and specific multimode concepts.
AB - Multimode propulsion is the integration of two or more propulsive modes into a single spacecraft propulsion system. In a multimode propulsion system, the key attribute is shared propellant between the different propulsive modes. Multimode propulsion is emerging as an enabling technology that promises enhanced capabilities for spacecraft and space missions, and can therefore play an important role in the future of in-space propulsion. Specifically, multimode propulsion has potential to provide unprecedented flexibility and adaptability to spacecraft, as well as provide mass savings for certain missions. These benefits extend to both medium and large spacecraft, as well as small satellites. Numerous multimode concepts have been explored and documented in the literature. Concepts combining cold gas, monopropellant, bipropellant, and solid chemical propulsion with electrothermal, electrostatic, and electromagnetic electric propulsion have all been investigated. Electrospray electric propulsion paired with monopropellant chemical propulsion has perhaps received the most recent attention. We review the concept of multimode propulsion, mission analyses, benefits, and specific multimode concepts.
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U2 - 10.2514/6.2019-4169
DO - 10.2514/6.2019-4169
M3 - Conference contribution
AN - SCOPUS:85095968594
SN - 9781624105906
T3 - AIAA Propulsion and Energy Forum and Exposition, 2019
BT - AIAA Propulsion and Energy Forum and Exposition, 2019
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Propulsion and Energy Forum and Exposition, 2019
Y2 - 19 August 2019 through 22 August 2019
ER -