Gossamer roadmap technology reference study for a solar polar mission

Malcolm Macdonald; Ciara McGrath; T Appourchaux; B. Dachwald; W Finsterle; L Gizon; P.C. Liewer; Colin McInnes; Giovanni Mengali; W. Seboldt; T Sekii; S.K. Solanki; M Velli; R.F. Wimmer-Schweingruber; Peter Spietz; Ruedeger Reinhard

doi:10.1007/978-3-642-34907-2_17

Gossamer roadmap technology reference study for a solar polar mission

Malcolm Macdonald, Ciara McGrath, T Appourchaux, B. Dachwald, W Finsterle, L Gizon, P.C. Liewer, Colin McInnes, Giovanni Mengali, W. Seboldt, T Sekii, S.K. Solanki, M Velli, R.F. Wimmer-Schweingruber, Peter Spietz, Ruedeger Reinhard

Mechanical And Aerospace Engineering

Research output: Chapter in Book/Report/Conference proceeding › Chapter (peer-reviewed)

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Abstract

A technology reference study for a solar polar mission is presented. The study uses novel analytical methods to quantify the mission design space including the required sail performance to achieve a given solar polar observation angle within a given timeframe and thus to derive mass allocations for the remaining spacecraft sub-systems, that is excluding the solar sail sub-system. A parametric, bottom-up, system mass budget analysis is then used to establish the required sail technology to deliver a range of science payloads, and to establish where such payloads can be delivered to within a given timeframe. It is found that a solar polar mission requires a solar sail of side-length 100 – 125 m to deliver a ‘sufficient value’ minimum science payload, and that a 2. 5μm sail film substrate is typically required, however the design is much less sensitive to the boom specific mass.

Original language	English
Title of host publication	Advances in Solar Sailing
Editors	Malcolm Macdonald
Place of Publication	Germany
Pages	243-258
Number of pages	16
Volume	1
DOIs	https://doi.org/10.1007/978-3-642-34907-2_17
Publication status	Published - Mar 2014
Event	3rd International Symposium on Solar Sailing - Glasgow, United Kingdom Duration: 11 Jun 2013 → 13 Jun 2013

Publication series

Name	Springer Praxis Books: Astronautical Engineering
Publisher	Springer Berlin Heidelberg
Volume	1

Conference

Conference	3rd International Symposium on Solar Sailing
Country/Territory	United Kingdom
City	Glasgow
Period	11/06/13 → 13/06/13

Keywords

gossamer roadmap technology
space weather
solar polar mission
solar sailing
space science
advanced propulsion
advanced space concepts
space technology

Access to Document

10.1007/978-3-642-34907-2_17

Macdonald M et al - Pure - Gossamer roadmap technology reference study for a solar polar mission Mar 2014Submitted manuscript, 0.99 MB

Cite this

Macdonald, M., McGrath, C., Appourchaux, T., Dachwald, B., Finsterle, W., Gizon, L., Liewer, P. C., McInnes, C., Mengali, G., Seboldt, W., Sekii, T., Solanki, S. K., Velli, M., Wimmer-Schweingruber, R. F., Spietz, P., & Reinhard, R. (2014). Gossamer roadmap technology reference study for a solar polar mission. In M. Macdonald (Ed.), Advances in Solar Sailing (Vol. 1, pp. 243-258). (Springer Praxis Books: Astronautical Engineering; Vol. 1).. https://doi.org/10.1007/978-3-642-34907-2_17

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abstract = "A technology reference study for a solar polar mission is presented. The study uses novel analytical methods to quantify the mission design space including the required sail performance to achieve a given solar polar observation angle within a given timeframe and thus to derive mass allocations for the remaining spacecraft sub-systems, that is excluding the solar sail sub-system. A parametric, bottom-up, system mass budget analysis is then used to establish the required sail technology to deliver a range of science payloads, and to establish where such payloads can be delivered to within a given timeframe. It is found that a solar polar mission requires a solar sail of side-length 100 – 125 m to deliver a {\textquoteleft}sufficient value{\textquoteright} minimum science payload, and that a 2. 5μm sail film substrate is typically required, however the design is much less sensitive to the boom specific mass. ",

keywords = "gossamer roadmap technology, space weather, solar polar mission, solar sailing, space science, advanced propulsion, advanced space concepts, space technology",

author = "Malcolm Macdonald and Ciara McGrath and T Appourchaux and B. Dachwald and W Finsterle and L Gizon and P.C. Liewer and Colin McInnes and Giovanni Mengali and W. Seboldt and T Sekii and S.K. Solanki and M Velli and R.F. Wimmer-Schweingruber and Peter Spietz and Ruedeger Reinhard",

year = "2014",

month = mar,

doi = "10.1007/978-3-642-34907-2\_17",

language = "English",

isbn = "9783642349065",

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series = "Springer Praxis Books: Astronautical Engineering",

publisher = "Springer Berlin Heidelberg",

pages = "243--258",

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booktitle = "Advances in Solar Sailing",

note = "3rd International Symposium on Solar Sailing ; Conference date: 11-06-2013 Through 13-06-2013",

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Macdonald, M, McGrath, C, Appourchaux, T, Dachwald, B, Finsterle, W, Gizon, L, Liewer, PC, McInnes, C, Mengali, G, Seboldt, W, Sekii, T, Solanki, SK, Velli, M, Wimmer-Schweingruber, RF, Spietz, P & Reinhard, R 2014, Gossamer roadmap technology reference study for a solar polar mission. in M Macdonald (ed.), Advances in Solar Sailing. vol. 1, Springer Praxis Books: Astronautical Engineering, vol. 1, Germany, pp. 243-258, 3rd International Symposium on Solar Sailing, Glasgow, United Kingdom, 11/06/13. https://doi.org/10.1007/978-3-642-34907-2_17

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AU - Appourchaux, T

AU - Dachwald, B.

AU - Finsterle, W

AU - Gizon, L

AU - Liewer, P.C.

AU - McInnes, Colin

AU - Mengali, Giovanni

AU - Seboldt, W.

AU - Sekii, T

AU - Solanki, S.K.

AU - Velli, M

AU - Wimmer-Schweingruber, R.F.

AU - Spietz, Peter

AU - Reinhard, Ruedeger

PY - 2014/3

Y1 - 2014/3

N2 - A technology reference study for a solar polar mission is presented. The study uses novel analytical methods to quantify the mission design space including the required sail performance to achieve a given solar polar observation angle within a given timeframe and thus to derive mass allocations for the remaining spacecraft sub-systems, that is excluding the solar sail sub-system. A parametric, bottom-up, system mass budget analysis is then used to establish the required sail technology to deliver a range of science payloads, and to establish where such payloads can be delivered to within a given timeframe. It is found that a solar polar mission requires a solar sail of side-length 100 – 125 m to deliver a ‘sufficient value’ minimum science payload, and that a 2. 5μm sail film substrate is typically required, however the design is much less sensitive to the boom specific mass.

AB - A technology reference study for a solar polar mission is presented. The study uses novel analytical methods to quantify the mission design space including the required sail performance to achieve a given solar polar observation angle within a given timeframe and thus to derive mass allocations for the remaining spacecraft sub-systems, that is excluding the solar sail sub-system. A parametric, bottom-up, system mass budget analysis is then used to establish the required sail technology to deliver a range of science payloads, and to establish where such payloads can be delivered to within a given timeframe. It is found that a solar polar mission requires a solar sail of side-length 100 – 125 m to deliver a ‘sufficient value’ minimum science payload, and that a 2. 5μm sail film substrate is typically required, however the design is much less sensitive to the boom specific mass.

KW - gossamer roadmap technology

KW - space weather

KW - solar polar mission

KW - solar sailing

KW - space science

KW - advanced propulsion

KW - advanced space concepts

KW - space technology

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DO - 10.1007/978-3-642-34907-2_17

M3 - Chapter (peer-reviewed)

SN - 9783642349065

VL - 1

T3 - Springer Praxis Books: Astronautical Engineering

SP - 243

EP - 258

BT - Advances in Solar Sailing

A2 - Macdonald, Malcolm

CY - Germany

T2 - 3rd International Symposium on Solar Sailing

Y2 - 11 June 2013 through 13 June 2013

ER -

Gossamer roadmap technology reference study for a solar polar mission

Abstract

Publication series

Conference

Keywords

Access to Document

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VISIONSPACE - VISIONARY SPACE SYSTEMS: ORBITAL DYNAMICS AT EXTREMES OF SPACECRAFT LENGTH SCALE (ERC ADVANCED GRANT)

Cite this

Gossamer roadmap technology reference study for a solar polar mission

Abstract

Publication series

Conference

Keywords

Access to Document

Other files and links

Fingerprint

Projects

VISIONSPACE - VISIONARY SPACE SYSTEMS: ORBITAL DYNAMICS AT EXTREMES OF SPACECRAFT LENGTH SCALE (ERC ADVANCED GRANT)

Cite this