Preliminary analysis and design of powered earth-mars cycling trajectories

K. Joseph Chen; Damon F. Landau; T. Troy Mcconaghy; Masataka Okutsu; James M. Longuski; Buzz Aldrin

Preliminary analysis and design of powered earth-mars cycling trajectories

K. Joseph Chen
, Damon F. Landau
, T. Troy Mcconaghy
, Masataka Okutsu
, James M. Longuski
, Buzz Aldrin

Division of Engineering and Science (Abington)

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution

22 Scopus citations

Abstract

We discuss preliminary results on constructing a powered cycler from semi-cycler trajectories. We present a powered cycler with reasonable transfer times and low encounter velocities. In addition, we develop a metric for evaluating cycler designs in comparison to other mission-to-Mars scenarios. The metric suggests that as vehicle mass (with respect to propellant mass) increases, the most advantageous system progresses from a "Design Reference Mission" scenario to Semi-Cyclers to Cyclers, which is highly indicative of how a human Mars transportation system might evolve.

Original language	English (US)
Title of host publication	AIAA/AAS Astrodynamics Specialist Conference and Exhibit
Publisher	American Institute of Aeronautics and Astronautics Inc.
ISBN (Print)	9781624101243
State	Published - Jan 1 2002
Event	AIAA/AAS Astrodynamics Specialist Conference and Exhibit 2002 - Monterey, CA, United States Duration: Aug 5 2002 → Aug 8 2002

Other

Other	AIAA/AAS Astrodynamics Specialist Conference and Exhibit 2002
Country/Territory	United States
City	Monterey, CA
Period	8/5/02 → 8/8/02

All Science Journal Classification (ASJC) codes

Astronomy and Astrophysics

Cite this

@inproceedings{c06542b49c8e45bfb5ddc5e66cf8a235,

title = "Preliminary analysis and design of powered earth-mars cycling trajectories",

abstract = "We discuss preliminary results on constructing a powered cycler from semi-cycler trajectories. We present a powered cycler with reasonable transfer times and low encounter velocities. In addition, we develop a metric for evaluating cycler designs in comparison to other mission-to-Mars scenarios. The metric suggests that as vehicle mass (with respect to propellant mass) increases, the most advantageous system progresses from a {"}Design Reference Mission{"} scenario to Semi-Cyclers to Cyclers, which is highly indicative of how a human Mars transportation system might evolve.",

author = "Chen, \{K. Joseph\} and Landau, \{Damon F.\} and Mcconaghy, \{T. Troy\} and Masataka Okutsu and Longuski, \{James M.\} and Buzz Aldrin",

year = "2002",

month = jan,

day = "1",

language = "English (US)",

isbn = "9781624101243",

booktitle = "AIAA/AAS Astrodynamics Specialist Conference and Exhibit",

publisher = "American Institute of Aeronautics and Astronautics Inc.",

note = "AIAA/AAS Astrodynamics Specialist Conference and Exhibit 2002 ; Conference date: 05-08-2002 Through 08-08-2002",

}

Chen, KJ, Landau, DF, Mcconaghy, TT, Okutsu, M, Longuski, JM & Aldrin, B 2002, Preliminary analysis and design of powered earth-mars cycling trajectories. in AIAA/AAS Astrodynamics Specialist Conference and Exhibit. American Institute of Aeronautics and Astronautics Inc., AIAA/AAS Astrodynamics Specialist Conference and Exhibit 2002, Monterey, CA, United States, 8/5/02.

TY - GEN

T1 - Preliminary analysis and design of powered earth-mars cycling trajectories

AU - Chen, K. Joseph

AU - Landau, Damon F.

AU - Mcconaghy, T. Troy

AU - Okutsu, Masataka

AU - Longuski, James M.

AU - Aldrin, Buzz

PY - 2002/1/1

Y1 - 2002/1/1

N2 - We discuss preliminary results on constructing a powered cycler from semi-cycler trajectories. We present a powered cycler with reasonable transfer times and low encounter velocities. In addition, we develop a metric for evaluating cycler designs in comparison to other mission-to-Mars scenarios. The metric suggests that as vehicle mass (with respect to propellant mass) increases, the most advantageous system progresses from a "Design Reference Mission" scenario to Semi-Cyclers to Cyclers, which is highly indicative of how a human Mars transportation system might evolve.

AB - We discuss preliminary results on constructing a powered cycler from semi-cycler trajectories. We present a powered cycler with reasonable transfer times and low encounter velocities. In addition, we develop a metric for evaluating cycler designs in comparison to other mission-to-Mars scenarios. The metric suggests that as vehicle mass (with respect to propellant mass) increases, the most advantageous system progresses from a "Design Reference Mission" scenario to Semi-Cyclers to Cyclers, which is highly indicative of how a human Mars transportation system might evolve.

UR - https://www.scopus.com/pages/publications/85086493103

UR - https://www.scopus.com/pages/publications/85086493103#tab=citedBy

M3 - Conference contribution

SN - 9781624101243

BT - AIAA/AAS Astrodynamics Specialist Conference and Exhibit

PB - American Institute of Aeronautics and Astronautics Inc.

T2 - AIAA/AAS Astrodynamics Specialist Conference and Exhibit 2002

Y2 - 5 August 2002 through 8 August 2002

ER -

Preliminary analysis and design of powered earth-mars cycling trajectories

Abstract

Other

All Science Journal Classification (ASJC) codes

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