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NASA NTRS · 20260005218

Mars Sample Retrieval Lander Thermal Protection System Design

Hannah Alpert·Josh Monk·Milad Mahzari·Suman Muppidi
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Abstract

The Mars Sample Return (MSR) Sample Retrieval Lander (SRL) was slated to launch in 2031 and enter Mars’ atmosphere after a 15-month cruise. After several iterations of vehicle design and trajectories, the latest mission architecture included a 4.72-meter diameter entry capsule entering the Martian atmosphere at 8 km/s, marking a 3.5x increase in kinetic energy when entering the atmosphere in comparison to Mars 2020. Designed to be the heaviest and fastest vehicle to enter Mars’ atmosphere, SRL required slim mass margins, and as such, the thermal protection system (TPS) design methodology needed to be tailored appropriately. The entry capsule aeroshell is composed of a heatshield, backshell, parachute support cone, and parachute lid, as shown in Fig. 1.

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Hannah Alpert, Josh Monk, Milad Mahzari, Suman Muppidi. Mars Sample Retrieval Lander Thermal Protection System Design. https://ntrs.nasa.gov/citations/20260005218

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