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the claim

Radiation pressure from the Sun affects spacecraft trajectories.

the verdict
SUPPORTED
the evidence backs this
Recorded sources
6 sources for · 0 against

Counts group repeated records of the same source within each side. They do not measure evidence strength or source independence.

Is it true that radiation pressure from the Sun affects spacecraft trajectories?

Yes. A reference article states that solar radiation pressure significantly affects the orbits and trajectories of all spacecraft, and several orbital-dynamics papers model solar radiation pressure as a perturbation on specific spacecraft trajectories.

Verdict: SUPPORTED · 6 sources for, 0 against · Last checked

The private library was unavailable for some searches in this check. Missing library results are not evidence against the claim.

Evidence for · 6
Radiation pressure
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Radiation pressure. (n.d.). en.wikipedia.org. https://en.wikipedia.org/wiki/Radiation_pressure

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More for · 5
Solar Radiation Pressure and Deviations from Keplerian Orbits
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Solar Radiation Pressure and Deviations from Keplerian Orbits. (n.d.). arxiv.org. https://arxiv.org/html/0901.1606v2

Attitude Dynamics of the Classical Dumbbell Problem with Solar Radiation Pressure
2015
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Attitude Dynamics of the Classical Dumbbell Problem with Solar Radiation Pressure. (2015). doi.org. https://doi.org/10.2514/1.g000392

Some Results of Adding Solar Radiation Pressure Force to the Restricted Three-Body Problem
1991
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Some Results of Adding Solar Radiation Pressure Force to the Restricted Three-Body Problem. (1991). doi.org. https://doi.org/10.21236/ada241397

IAC-18.C1.2.9 WIDE-FIELD INFRARED SURVEY TELESCOPE AND STARSHADE FORMATION FLYING DYNAMICS AT SUN-EARTH L2
2018
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IAC-18.C1.2.9 WIDE-FIELD INFRARED SURVEY TELESCOPE AND STARSHADE FORMATION FLYING DYNAMICS AT SUN-EARTH L2. (2018). doi.org. https://doi.org/10.13016/m2t43j66t

Real-time control of optimal low-thrust transfer to the Sun-Earth L1 halo orbit in the bicircular four-body problem
2011
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Real-time control of optimal low-thrust transfer to the Sun-Earth L1 halo orbit in the bicircular four-body problem. (2011). inria.hal.science. https://doi.org/10.1016/j.actaastro.2011.05.017

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