DSIAC was asked for information pertaining to the capability of current EMRG systems to support the launch of objects, mainly SmallSats in the CubeSat/nanosatellite to femtosatellite class. Their masses must range from 0.01 kg to 10 kg, from the Earth to LEO and from the Moon’s surface to a Mars transfer orbit. A DSIAC subject matter expert in propulsion systems at The Johns Hopkins University Energetics Research Group provided commentary on the capabilities and issues with using an EMRG in such a manner and reference documents.
Using Electromagnetic Railguns to Launch Small Satellites to Low Earth Orbit
Posted on May 27, 2020 | Completed on March 31, 2020 | By: Benjamin Hill-lam
What modeling or testing has been done on using electromagnetic railguns (EMRGs) for launching low Earth orbit (LEO) projectiles?
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