Design optimisation and analysis of very high power transportation system to Mars

Christie Maddock; Ben Parsonage; Lorenzo Angelo Ricciardi; Massimiliano Vasile; Orr Cohen

Design optimisation and analysis of very high power transportation system to Mars

Christie Maddock, Ben Parsonage, Lorenzo Angelo Ricciardi, Massimiliano Vasile, Orr Cohen

Research output: Contribution to conference › Proceeding › peer-review

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Abstract

This paper presents a preliminary design for a crewed transportation system to Mars, looking at both the vehicle and mission design trade-offs. The mission requirements are for a return mission to Mars, with a variable stay time on/around the planet. The vehicle is designed for a minimum crew of 3 plus 50 t cargo, and assumes in-orbit assembly and re-fueling options. A nominal vehicle design was developed using a bimodal nuclear propulsion system. A multi-objective optimisation was run examining the trade-offs between flight times, and total duration, for different Mars stay times, planetary conjunction angles, dry masses and engine sizing, and the mission trajectories.

Original language	English
Number of pages	10
Publication status	Published - 25 Oct 2021
Event	72nd International Astronautical Congress - Dubai World Trade Centre, Dubai, United Arab Emirates Duration: 25 Oct 2021 → 29 Oct 2021 https://iac2021.org/ https://www.iafastro.org/events/iac/iac-2021/

Conference

Conference	72nd International Astronautical Congress
Abbreviated title	IAC 2021
Country/Territory	United Arab Emirates
City	Dubai
Period	25/10/21 → 29/10/21
Internet address	https://iac2021.org/ https://www.iafastro.org/events/iac/iac-2021/

Keywords

nuclear propulsion
Mars mission
design optimisation
mission analysis

UN SDGs

This output contributes to the following UN Sustainable Development Goals (SDGs)

Access to Document

Maddock-etal-IAC-2021-Design-optimisation-and-analysis-of-very-high-powerAccepted author manuscript, 922 KB

Cite this

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title = "Design optimisation and analysis of very high power transportation system to Mars",

abstract = "This paper presents a preliminary design for a crewed transportation system to Mars, looking at both the vehicle and mission design trade-offs. The mission requirements are for a return mission to Mars, with a variable stay time on/around the planet. The vehicle is designed for a minimum crew of 3 plus 50 t cargo, and assumes in-orbit assembly and re-fueling options. A nominal vehicle design was developed using a bimodal nuclear propulsion system. A multi-objective optimisation was run examining the trade-offs between flight times, and total duration, for different Mars stay times, planetary conjunction angles, dry masses and engine sizing, and the mission trajectories.",

keywords = "nuclear propulsion, Mars mission, design optimisation, mission analysis",

author = "Christie Maddock and Ben Parsonage and Ricciardi, {Lorenzo Angelo} and Massimiliano Vasile and Orr Cohen",

year = "2021",

month = oct,

day = "25",

language = "English",

note = "72nd International Astronautical Congress, IAC 2021 ; Conference date: 25-10-2021 Through 29-10-2021",

url = "https://iac2021.org/, https://www.iafastro.org/events/iac/iac-2021/",

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TY - CONF

T1 - Design optimisation and analysis of very high power transportation system to Mars

AU - Maddock, Christie

AU - Parsonage, Ben

AU - Ricciardi, Lorenzo Angelo

AU - Vasile, Massimiliano

AU - Cohen, Orr

PY - 2021/10/25

Y1 - 2021/10/25

N2 - This paper presents a preliminary design for a crewed transportation system to Mars, looking at both the vehicle and mission design trade-offs. The mission requirements are for a return mission to Mars, with a variable stay time on/around the planet. The vehicle is designed for a minimum crew of 3 plus 50 t cargo, and assumes in-orbit assembly and re-fueling options. A nominal vehicle design was developed using a bimodal nuclear propulsion system. A multi-objective optimisation was run examining the trade-offs between flight times, and total duration, for different Mars stay times, planetary conjunction angles, dry masses and engine sizing, and the mission trajectories.

AB - This paper presents a preliminary design for a crewed transportation system to Mars, looking at both the vehicle and mission design trade-offs. The mission requirements are for a return mission to Mars, with a variable stay time on/around the planet. The vehicle is designed for a minimum crew of 3 plus 50 t cargo, and assumes in-orbit assembly and re-fueling options. A nominal vehicle design was developed using a bimodal nuclear propulsion system. A multi-objective optimisation was run examining the trade-offs between flight times, and total duration, for different Mars stay times, planetary conjunction angles, dry masses and engine sizing, and the mission trajectories.

KW - nuclear propulsion

KW - Mars mission

KW - design optimisation

KW - mission analysis

UR - https://www.iafastro.org/events/iac/iac-2021/

M3 - Proceeding

T2 - 72nd International Astronautical Congress

Y2 - 25 October 2021 through 29 October 2021

ER -

Design optimisation and analysis of very high power transportation system to Mars

Abstract

Conference

Keywords

UN SDGs

Access to Document

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Assessment of a very high power cargo transportation system to Mars

ARCHIE-WeSt (UOSHPC)

Cite this

Design optimisation and analysis of very high power transportation system to Mars

Abstract

Conference

Keywords

UN SDGs

Access to Document

Other files and links

Fingerprint

Projects

Assessment of a very high power cargo transportation system to Mars

Equipment

ARCHIE-WeSt (UOSHPC)

Cite this