The use of deep space port at L1 and L2 points in Sun-Earth and Earth-Moon systems with low thrust departure / return flight strategy

Jun'ichiro Kawaguchi; Kohta Tarao; Michihiro Matsumoto; Mutsuko Morimoto

The use of deep space port at L1 and L2 points in Sun-Earth and Earth-Moon systems with low thrust departure / return flight strategy

Jun'ichiro Kawaguchi, Kohta Tarao, Michihiro Matsumoto, Mutsuko Morimoto

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

Abstract

This paper presents how the collinear libration points in Sun-Earth and Earth-Moon systems are useful as space infrastructures designated here Deep Space Ports. This paper presents how the future deep space traffic system will be by contemplating the vicinity around the L1/L2 points as the quays in the Sun-Earth/Earth-Moon systems. Here is presented the Electric Delta-V Earth Gravity Assist technique, with the artificial small Halo orbits in the vicinity of those libration points. They are maintained by the low thrust propulsion means all the time to draw concise circular loci around the equilibrium points.

Original language	English
Title of host publication	International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008
Pages	2090-2102
Number of pages	13
Publication status	Published - 2008
Externally published	Yes
Event	59th International Astronautical Congress 2008, IAC 2008 - Glasgow, United Kingdom Duration: 2008 Sept 29 → 2008 Oct 3

Publication series

Name	International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008
Volume	4

Other

Other	59th International Astronautical Congress 2008, IAC 2008
Country/Territory	United Kingdom
City	Glasgow
Period	08/9/29 → 08/10/3

ASJC Scopus subject areas

Space and Planetary Science
Aerospace Engineering
Astronomy and Astrophysics

Cite this

Kawaguchi, J., Tarao, K., Matsumoto, M., & Morimoto, M. (2008). The use of deep space port at L1 and L2 points in Sun-Earth and Earth-Moon systems with low thrust departure / return flight strategy. In International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008 (pp. 2090-2102). (International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008; Vol. 4).

The use of deep space port at L1 and L2 points in Sun-Earth and Earth-Moon systems with low thrust departure / return flight strategy. / Kawaguchi, Jun'ichiro; Tarao, Kohta; Matsumoto, Michihiro et al.
International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008. 2008. p. 2090-2102 (International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008; Vol. 4).

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

Kawaguchi, J, Tarao, K, Matsumoto, M & Morimoto, M 2008, The use of deep space port at L1 and L2 points in Sun-Earth and Earth-Moon systems with low thrust departure / return flight strategy. in International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008. International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008, vol. 4, pp. 2090-2102, 59th International Astronautical Congress 2008, IAC 2008, Glasgow, United Kingdom, 08/9/29.

Kawaguchi J, Tarao K, Matsumoto M, Morimoto M. The use of deep space port at L1 and L2 points in Sun-Earth and Earth-Moon systems with low thrust departure / return flight strategy. In International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008. 2008. p. 2090-2102. (International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008).

Kawaguchi, Jun'ichiro ; Tarao, Kohta ; Matsumoto, Michihiro et al. / The use of deep space port at L1 and L2 points in Sun-Earth and Earth-Moon systems with low thrust departure / return flight strategy. International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008. 2008. pp. 2090-2102 (International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008).

@inproceedings{57cc853530664b2f8060f08b23b47d4e,

title = "The use of deep space port at L1 and L2 points in Sun-Earth and Earth-Moon systems with low thrust departure / return flight strategy",

abstract = "This paper presents how the collinear libration points in Sun-Earth and Earth-Moon systems are useful as space infrastructures designated here Deep Space Ports. This paper presents how the future deep space traffic system will be by contemplating the vicinity around the L1/L2 points as the quays in the Sun-Earth/Earth-Moon systems. Here is presented the Electric Delta-V Earth Gravity Assist technique, with the artificial small Halo orbits in the vicinity of those libration points. They are maintained by the low thrust propulsion means all the time to draw concise circular loci around the equilibrium points.",

author = "Jun'ichiro Kawaguchi and Kohta Tarao and Michihiro Matsumoto and Mutsuko Morimoto",

year = "2008",

language = "English",

isbn = "9781615671601",

series = "International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008",

pages = "2090--2102",

booktitle = "International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008",

note = "59th International Astronautical Congress 2008, IAC 2008 ; Conference date: 29-09-2008 Through 03-10-2008",

}

TY - GEN

T1 - The use of deep space port at L1 and L2 points in Sun-Earth and Earth-Moon systems with low thrust departure / return flight strategy

AU - Kawaguchi, Jun'ichiro

AU - Tarao, Kohta

AU - Matsumoto, Michihiro

AU - Morimoto, Mutsuko

PY - 2008

Y1 - 2008

N2 - This paper presents how the collinear libration points in Sun-Earth and Earth-Moon systems are useful as space infrastructures designated here Deep Space Ports. This paper presents how the future deep space traffic system will be by contemplating the vicinity around the L1/L2 points as the quays in the Sun-Earth/Earth-Moon systems. Here is presented the Electric Delta-V Earth Gravity Assist technique, with the artificial small Halo orbits in the vicinity of those libration points. They are maintained by the low thrust propulsion means all the time to draw concise circular loci around the equilibrium points.

AB - This paper presents how the collinear libration points in Sun-Earth and Earth-Moon systems are useful as space infrastructures designated here Deep Space Ports. This paper presents how the future deep space traffic system will be by contemplating the vicinity around the L1/L2 points as the quays in the Sun-Earth/Earth-Moon systems. Here is presented the Electric Delta-V Earth Gravity Assist technique, with the artificial small Halo orbits in the vicinity of those libration points. They are maintained by the low thrust propulsion means all the time to draw concise circular loci around the equilibrium points.

UR - http://www.scopus.com/inward/record.url?scp=77950464693&partnerID=8YFLogxK

UR - http://www.scopus.com/inward/citedby.url?scp=77950464693&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:77950464693

SN - 9781615671601

T3 - International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008

SP - 2090

EP - 2102

BT - International Astronautical Federation - 59th International Astronautical Congress 2008, IAC 2008

T2 - 59th International Astronautical Congress 2008, IAC 2008

Y2 - 29 September 2008 through 3 October 2008

ER -

The use of deep space port at L1 and L2 points in Sun-Earth and Earth-Moon systems with low thrust departure / return flight strategy

Abstract

Publication series

Other

ASJC Scopus subject areas

Other files and links

Fingerprint

Cite this