Cited by 7Spacecraft Dynamics and ControlPlanetary Science and ExplorationSpacecraft Design and Technology

3 months transit time to Mars for human missions using SpaceX Starship

Open access
Kingdon, Jack·2025·Scientific Reports

Abstract

Historically, spacecraft have followed trajectories that took between six and nine months to reach Mars, using traditional chemical propulsion on roughly Hohmann transfers. It is commonly believed that advances in propulsion technology, such as nuclear thermal or VASIMR, are necessary to reduce that transit time. In this paper, we show the feasibility of transit to Mars using the SpaceX Starship taking 90 days. We outline two trajectories that reduce each transit to between 90 and 104 days each way. These trajectories are within NASA career radiation limits, while 180-day trajectories are not.

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Research works printed but not linked: 4

  1. [10]Stark, A. et al. ECI Modular Assembled Radiators for NEP Vehicles (MARVL), an Overview. In Thermal & Fluids Analysis Workshop (TFAWS 2024) (NASA Glenn Research Center, Cleveland, OH, 2024) (accessed 24 Feb 2025).
  2. [14]Musk, E. Tweet from Elon Musk on January 17, 2020 (2020). https://x.com/elonmusk/status/1217989066181898240 (accessed 31 Dec 2024).
  3. [31]Musk, E. Tweet from Elon Musk on January 11, 2020 (2020). https://x.com/elonmusk/status/1215719463913345024 (accessed 31 Dec 2024).
  4. [54]SpaceX. Tweet from SpaceX on Aug 3, 2024 (2024). https://x.com/SpaceX/status/1819772716339339664 (accessed 31 Dec 2024).

Authors
Kingdon, J.
Affiliations
University of California, Santa Barbara (US)
Corresponding author
Kingdon, Jack
Venue
Scientific Reports
Published
2025-05-22
Volume
15
Issue
1
Pages
17764-17764
ISSN
2045-2322 (ISSN-L)
OpenAlex
W4410586840
Cited by
4
References
13
Citations by year
2026: 2 · 2025: 2
FWCI
1.50
Type
journal article
Language
en
Open access
Locations
  • Scientific Reports (publishedVersion, cc-by)
  • PubMed Central (publishedVersion, cc-by)
  • PubMed (publishedVersion)
  • DOAJ (DOAJ: Directory of Open Access Journals) (submittedVersion, cc-by-sa)
Topics
  • Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Dynamics and Control
  • Physical Sciences › Physics and Astronomy › Astronomy and Astrophysics › Planetary Science and Exploration
  • Physical Sciences › Engineering › Aerospace Engineering › Spacecraft Design and Technology
Keywords
Mars transit, human Mars missions, transit time reduction, trajectory optimization, Hohmann transfer, nuclear thermal propulsion, VASIMR, radiation exposure, chemical propulsion

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