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Red Dragon Drill Missions to Mars

Authors :
Jennifer L Heldmann
Carol R Stoker
Andrew Gonzales
Christopher P Mckay
Alfonso Davila
Brian J Glass
Larry Lemke
Gale Paulsen
David Wilson
Kris Zacny
Source :
Acta Astronautica. 141
Publication Year :
2017
Publisher :
United States: NASA Center for Aerospace Information (CASI), 2017.

Abstract

We present the concept of using a variant of a Space Exploration Technologies Corporation (SpaceX) Dragon space capsule as a low-cost, large-capacity, near-term, Mars lander (dubbed "Red Dragon") for scientific and human precursor missions. SpaceX initially designed the Dragon capsule for flight near Earth, and Dragon has successfully flown many times to low-Earth orbit (LEO) and successfully returned the Dragon spacecraft to Earth. Here we present capsule hardware modifications that are required to enable flight to Mars and operations on the martian surface. We discuss the use of the Dragon system to support NASA Discovery class missions to Mars and focus in particular on Dragon's applications for drilling missions. We find that a Red Dragon platform is well suited for missions capable of drilling deeper on Mars (at least 2 m) than has been accomplished to date due to its ability to land in a powered controlled mode, accommodate a long drill string, and provide payload space for sample processing and analysis. We show that a Red Dragon drill lander could conduct surface missions at three possible targets including the ice-cemented ground at the Phoenix landing site (68degN), the subsurface ice discovered near the Viking 2 (49degN) site by fresh impact craters, and the dark sedimentary subsurface material at the Curiosity site (4.5degS).

Details

Language :
English
ISSN :
00945765
Volume :
141
Database :
NASA Technical Reports
Journal :
Acta Astronautica
Publication Type :
Report
Accession number :
edsnas.20170012502
Document Type :
Report
Full Text :
https://doi.org/10.1016/j.actaastro.2017.10.002