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Reduction of Martian Sample Return Mission Launch Mass with Solar Sail Propulsion

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Abstract

Solar sails have the potential to provide mass and cost savings for spacecraft traveling within the inner solar system. Companies like L’Garde have demonstrated sail manufacturability and various in-space deployment methods. The purpose of this study was to evaluate a current Mars sample return architecture and to determine how cost and mass would be reduced by incorporating a solar sail propulsion system. The team validated the design proposed by L’Garde, and scaled the design based on a trajectory analysis. Using the solar sail design reduced the required mass, eliminating one of the three launches required in the original architecture.

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Abbreviations

ACO:

Advanced Concepts Office

ACS:

Attitude Control System

AR&C:

Arrival, Rendezvous & Capture

C&DH:

Command & Data Handling

CP1:

Colorless Polymer 1

EEV:

Earth Entry Vehicle

ERS:

Earth Return Stage

GN&C:

Guidance Navigation and Control

GR&A:

Ground Rules and Assumptions

GSD:

Ground System Demonstration

HGA:

High Gain Antenna

IEM:

Integrated Electronics Module

Isp:

Specific Impulse

JPL:

Jet Propulsion Laboratory

LEO:

Low Earth Orbit

LGA:

Low Gain Antenna

MEL:

Master Equipment List

MIDAS:

Mission Design and Analysis Software

MLI:

Multi-Layer Insulation

MOI:

Mars Orbit Insertion

MPDM:

Multi-Purpose Data Module

MPS:

Main Propulsion System

MSFC:

Marshall Space Flight Center

MSR:

Mars Exploration Sample Return

NASA:

National Aeronautics and Space Administration

ORU:

Orbital Replacement Unit

OS:

Orbiting Sample

PDU:

Power Distribution Unit

PMAD:

Power Management and Distribution

SBC:

Single Board Computer

SRO:

Sample Return Orbiter

SSPA:

Solid State Power Amplifier

TRL:

Technology Readiness Level

UHF:

Ultra High Frequency

References

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Correspondence to Tiffany E. Russell .

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© 2014 Springer-Verlag Berlin Heidelberg

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Russell, T.E. et al. (2014). Reduction of Martian Sample Return Mission Launch Mass with Solar Sail Propulsion. In: Macdonald, M. (eds) Advances in Solar Sailing. Springer Praxis Books(). Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-34907-2_21

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  • DOI: https://doi.org/10.1007/978-3-642-34907-2_21

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  • Publisher Name: Springer, Berlin, Heidelberg

  • Print ISBN: 978-3-642-34906-5

  • Online ISBN: 978-3-642-34907-2

  • eBook Packages: EngineeringEngineering (R0)

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