Photon Spacecraft and Aerocapture: Enabling Small Low-Circular Orbiters at Mars and Venus
Athul Pradeepkumar Girija

TL;DR
This paper explores how drag modulation aerocapture can enable small spacecraft to achieve low-circular orbits around Mars and Venus, reducing propellant needs and costs for small missions.
Contribution
It demonstrates the feasibility of combining Photon spacecraft with drag modulation aerocapture to enable low-orbit insertion for small satellites at Mars and Venus.
Findings
Drag modulation aerocapture reduces propellant requirements for orbit insertion.
Photon spacecraft can deliver small orbiters to low-circular orbits using aerocapture.
Mass and cost savings enable frequent small satellite missions at Mars and Venus.
Abstract
With advancements in low-cost launchers and small interplanetary spacecraft, NASA has recognized the potential of small missions to perform focused planetary science investigations at Mars and Venus. The EscaPADE, part of the NASA SIMPLEx program will deliver two small spacecraft to elliptical orbits around Mars using the Photon spacecraft. Orbit insertion, particularly to low-circular orbits requires significant propellant, taking up a substantial fraction of the Photon wet mass and present a significant challenge for small missions. The large V requirements for low-circular orbit make it difficult to insert small satellites into these orbits even with the highly capable Photon, as the total V for Earth escape and orbit insertion exceeds its capability. Drag modulation aerocapture offers a promising alternative, using the atmospheric drag to obtain the large V.…
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Taxonomy
TopicsSpacecraft Dynamics and Control · Planetary Science and Exploration · Space Satellite Systems and Control
