Trajectory options for human mars missions

Paul D. Wooster, Robert D. Braun, Jaemyung Ahn, Zachary R. Putnam

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

This paper explores trajectory options for the human exploration of Mars, with an emphasis on conjunction-class missions. Conjunction-class missions are characterized by short in-space durations with long surface stays, as opposed to the long in-space durations and short surface stays characteristic of opposition-class missions. Earth-Mars and Mars-Earth trajectories are presented across a series of mission opportunities and transfer times in order to explore the space of possible crew and cargo transfer trajectories. In the specific instance of crew transfer from Earth to Mars, the potential for aborting the mission without capture into Mars orbit is also of interest. As such two additional classes of trajectories are considered: free-return trajectories, where the trajectory would return the crew to Earth after a fixed period of time; and propulsive-abort trajectories, where the propulsive capability of the transfer vehicle is used to modify the trajectory during a Mars swing-by. The propulsive requirements of a trajectory, due to their associated impact on spacecraft mass, are clearly of interest in assessing trajectories for human Mars missions. Beyond the propulsive requirements, trajectory selection can have a significant impact on the entry velocity and therefore the aeroassist system requirements. The paper suggests potential constraints for entry velocities at Earth and Mars. Based upon Mars entry velocity, the 2-year period free-return abort trajectory is shown to be less desirable than previously considered for many mission opportunities.

Original languageEnglish (US)
Title of host publicationCollection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006
Pages835-851
Number of pages17
StatePublished - Dec 1 2006
Externally publishedYes
EventAIAA/AAS Astrodynamics Specialist Conference, 2006 - Keystone, CO, United States
Duration: Aug 21 2006Aug 24 2006

Publication series

NameCollection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006
Volume2

Other

OtherAIAA/AAS Astrodynamics Specialist Conference, 2006
CountryUnited States
CityKeystone, CO
Period8/21/068/24/06

Fingerprint

Trajectories
Earth (planet)
Aeroassist
Spacecraft
Orbits

ASJC Scopus subject areas

  • Engineering(all)

Cite this

Wooster, P. D., Braun, R. D., Ahn, J., & Putnam, Z. R. (2006). Trajectory options for human mars missions. In Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006 (pp. 835-851). (Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006; Vol. 2).

Trajectory options for human mars missions. / Wooster, Paul D.; Braun, Robert D.; Ahn, Jaemyung; Putnam, Zachary R.

Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006. 2006. p. 835-851 (Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006; Vol. 2).

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Wooster, PD, Braun, RD, Ahn, J & Putnam, ZR 2006, Trajectory options for human mars missions. in Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006. Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006, vol. 2, pp. 835-851, AIAA/AAS Astrodynamics Specialist Conference, 2006, Keystone, CO, United States, 8/21/06.
Wooster PD, Braun RD, Ahn J, Putnam ZR. Trajectory options for human mars missions. In Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006. 2006. p. 835-851. (Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006).
Wooster, Paul D. ; Braun, Robert D. ; Ahn, Jaemyung ; Putnam, Zachary R. / Trajectory options for human mars missions. Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006. 2006. pp. 835-851 (Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006).
@inproceedings{62e1a6169d134e8e9bcfca728c6b64a1,
title = "Trajectory options for human mars missions",
abstract = "This paper explores trajectory options for the human exploration of Mars, with an emphasis on conjunction-class missions. Conjunction-class missions are characterized by short in-space durations with long surface stays, as opposed to the long in-space durations and short surface stays characteristic of opposition-class missions. Earth-Mars and Mars-Earth trajectories are presented across a series of mission opportunities and transfer times in order to explore the space of possible crew and cargo transfer trajectories. In the specific instance of crew transfer from Earth to Mars, the potential for aborting the mission without capture into Mars orbit is also of interest. As such two additional classes of trajectories are considered: free-return trajectories, where the trajectory would return the crew to Earth after a fixed period of time; and propulsive-abort trajectories, where the propulsive capability of the transfer vehicle is used to modify the trajectory during a Mars swing-by. The propulsive requirements of a trajectory, due to their associated impact on spacecraft mass, are clearly of interest in assessing trajectories for human Mars missions. Beyond the propulsive requirements, trajectory selection can have a significant impact on the entry velocity and therefore the aeroassist system requirements. The paper suggests potential constraints for entry velocities at Earth and Mars. Based upon Mars entry velocity, the 2-year period free-return abort trajectory is shown to be less desirable than previously considered for many mission opportunities.",
author = "Wooster, {Paul D.} and Braun, {Robert D.} and Jaemyung Ahn and Putnam, {Zachary R.}",
year = "2006",
month = "12",
day = "1",
language = "English (US)",
isbn = "1563478226",
series = "Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006",
pages = "835--851",
booktitle = "Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006",

}

TY - GEN

T1 - Trajectory options for human mars missions

AU - Wooster, Paul D.

AU - Braun, Robert D.

AU - Ahn, Jaemyung

AU - Putnam, Zachary R.

PY - 2006/12/1

Y1 - 2006/12/1

N2 - This paper explores trajectory options for the human exploration of Mars, with an emphasis on conjunction-class missions. Conjunction-class missions are characterized by short in-space durations with long surface stays, as opposed to the long in-space durations and short surface stays characteristic of opposition-class missions. Earth-Mars and Mars-Earth trajectories are presented across a series of mission opportunities and transfer times in order to explore the space of possible crew and cargo transfer trajectories. In the specific instance of crew transfer from Earth to Mars, the potential for aborting the mission without capture into Mars orbit is also of interest. As such two additional classes of trajectories are considered: free-return trajectories, where the trajectory would return the crew to Earth after a fixed period of time; and propulsive-abort trajectories, where the propulsive capability of the transfer vehicle is used to modify the trajectory during a Mars swing-by. The propulsive requirements of a trajectory, due to their associated impact on spacecraft mass, are clearly of interest in assessing trajectories for human Mars missions. Beyond the propulsive requirements, trajectory selection can have a significant impact on the entry velocity and therefore the aeroassist system requirements. The paper suggests potential constraints for entry velocities at Earth and Mars. Based upon Mars entry velocity, the 2-year period free-return abort trajectory is shown to be less desirable than previously considered for many mission opportunities.

AB - This paper explores trajectory options for the human exploration of Mars, with an emphasis on conjunction-class missions. Conjunction-class missions are characterized by short in-space durations with long surface stays, as opposed to the long in-space durations and short surface stays characteristic of opposition-class missions. Earth-Mars and Mars-Earth trajectories are presented across a series of mission opportunities and transfer times in order to explore the space of possible crew and cargo transfer trajectories. In the specific instance of crew transfer from Earth to Mars, the potential for aborting the mission without capture into Mars orbit is also of interest. As such two additional classes of trajectories are considered: free-return trajectories, where the trajectory would return the crew to Earth after a fixed period of time; and propulsive-abort trajectories, where the propulsive capability of the transfer vehicle is used to modify the trajectory during a Mars swing-by. The propulsive requirements of a trajectory, due to their associated impact on spacecraft mass, are clearly of interest in assessing trajectories for human Mars missions. Beyond the propulsive requirements, trajectory selection can have a significant impact on the entry velocity and therefore the aeroassist system requirements. The paper suggests potential constraints for entry velocities at Earth and Mars. Based upon Mars entry velocity, the 2-year period free-return abort trajectory is shown to be less desirable than previously considered for many mission opportunities.

UR - http://www.scopus.com/inward/record.url?scp=33846041583&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=33846041583&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:33846041583

SN - 1563478226

SN - 9781563478222

T3 - Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006

SP - 835

EP - 851

BT - Collection of Technical Papers - AIAA/AAS Astrodynamics Specialist Conference, 2006

ER -