Solar thermal rocket (English Wikipedia)

Analysis of information sources in references of the Wikipedia article "Solar thermal rocket" in English language version.

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Byers, Woodcock (2003). "Evaluation of Solar Thermal Propulsion for In-Space Propulsion Application". 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Joint Propulsion Conferences. AIAA. doi:10.2514/6.2003-5029. ISBN 978-1-62410-098-7.

dlr.de

la.dlr.de

Webpage DLR Solar Thermal Propulsion of the Institut für Raumfahrtantriebe Abteilung Systemanalyse Raumtransport (SART) date = November 2006 Archived 2007-07-06 at the Wayback Machine

doi.org

Byers, Woodcock (2003). "Evaluation of Solar Thermal Propulsion for In-Space Propulsion Application". 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Joint Propulsion Conferences. AIAA. doi:10.2514/6.2003-5029. ISBN 978-1-62410-098-7.

nasa.gov

NASA. "Robotic Asteroid Prospector NIAC Phase 1 Final Report" (PDF). NASA. Retrieved March 11, 2021.

neofuel.com

Zuppero, Anthony (2005). "Propulsion to Moons of Jupiter Using Heat and Water Without Electrolysis Or Cryogenics" (PDF). Space Exploration 2005. SESI Conference Series. 001. Retrieved June 20, 2012.
Zuppero, Anthony. "new fuel: Near Earth Object fuel (Neofuel, using abundant off-earth resources for interplanetary transport)". Retrieved June 20, 2012.

newmars.com

"Interplanetary transportation» Solar Thermal Ground to Orbit - Solar Thermal Tech to launch". NewMars. Retrieved January 19, 2023.

nianet.org

bigidea.nianet.org

Zegler, Frank; Bernard Kutter (2010-09-02). "Evolving to a Depot-Based Space Transportation Architecture" (PDF). AIAA SPACE 2010 Conference & Exposition. AIAA. p. 3. Retrieved March 31, 2017. the waste hydrogen that has boiled off happens to be the best known propellant (as a monopropellant in a basic solar-thermal propulsion system) for this task. A practical depot must evolve hydrogen at a minimum rate that matches the station keeping demands.