Small-Body and Heliophysics Missions using Hybrid Low-Thrust Propulsion
Throughout the history of spaceflight, new missions and capabilities have been enabled by the development of increasingly efficient and powerful propulsion systems. However, all of these systems, from the earliest chemical engines to modern electric thrusters, require propellant, thereby reducing th...
Main Author: | Miller, Daniel |
---|---|
Other Authors: | Linares, Richard |
Format: | Thesis |
Published: |
Massachusetts Institute of Technology
2024
|
Online Access: | https://hdl.handle.net/1721.1/155391 |
Similar Items
-
Exploiting Laboratory and Heliophysics Plasma Synergies
by: Dahlburg, Jill, et al.
Published: (2011) -
Development of low-thrust solid rocket motors for small, fast aircraft propulsion
by: Vernacchia, Matthew T., et al.
Published: (2020) -
Development of low-thrust solid rocket motors for small, fast aircraft propulsion
by: Vernacchia, Matthew T.
Published: (2020) -
Low-Thrust Solid Rocket Motors for Small, Fast Aircraft Propulsion: Design and Development
by: Vernacchia, Matthew T., et al.
Published: (2021) -
Milli-Newton thrust stand for electric propulsion
by: Mirczak, Jareb D. (Jareb Douglas), 1979-
Published: (2013)