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NASA NTRS · 20140007403

Cubesat Application for Planetary Entry Missions (CAPE)

Esper, Jaime·Baumann, Jean-Pierre·Herdrich, Georg
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Abstract

The Cubesat Application for Planetary Entry Missions (CAPE) concept describes a high-performing Cubesat system which includes a propulsion module and miniaturized technologies capable of surviving atmospheric entry heating, while reliably transmitting scientific and engineering data. The Micro Return Capsule 2 (MIRKA2) is CAPE’s first planetary entry probe flight prototype. Within this context, this paper summarizes CAPE’s configuration and typical operational scenario. It also summarizes MIRKA2’s design and basic aerodynamic characteristics, and discusses potential challenges drawn from the experience of missions such as Stardust and MUSES-C. CAPE not only opens the door to new planetary mission capabilities, it also offers relatively low-cost opportunities especially suitable to university participation.

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BibTeXRIS

Esper, Jaime, Baumann, Jean-Pierre, Herdrich, Georg. 2013-06-20. Cubesat Application for Planetary Entry Missions (CAPE). https://ntrs.nasa.gov/citations/20140007403

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