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Controlled solar sail transfers into the near-sun orbits. / Koblik, V.; Polyakhova, E.; Sokolov, L.; Shmyrov, A.

In: Advances in Space Research, Vol. 29, No. 12, 01.01.2002, p. 2083-2088.

Research output: Contribution to journal › Article › peer-review

Harvard

Koblik, V, Polyakhova, E, Sokolov, L & Shmyrov, A 2002, 'Controlled solar sail transfers into the near-sun orbits', Advances in Space Research, vol. 29, no. 12, pp. 2083-2088. https://doi.org/10.1016/S0273-1177(02)00156-4

APA

Koblik, V., Polyakhova, E., Sokolov, L., & Shmyrov, A. (2002). Controlled solar sail transfers into the near-sun orbits. Advances in Space Research, 29(12), 2083-2088. https://doi.org/10.1016/S0273-1177(02)00156-4

Vancouver

Koblik V, Polyakhova E, Sokolov L, Shmyrov A. Controlled solar sail transfers into the near-sun orbits. Advances in Space Research. 2002 Jan 1;29(12):2083-2088. https://doi.org/10.1016/S0273-1177(02)00156-4

Author

Koblik, V. ; Polyakhova, E. ; Sokolov, L. ; Shmyrov, A. / Controlled solar sail transfers into the near-sun orbits. In: Advances in Space Research. 2002 ; Vol. 29, No. 12. pp. 2083-2088.

BibTeX

@article{d546e6e821a0408e800f4d36f86e45b5,
title = "Controlled solar sail transfers into the near-sun orbits",
abstract = "We present results of numerical simulations of trajectories of a space probe with a flat solar sail which moves from a circular Earth orbit to near-Sun regions. We consider the upper limit of the sail temperature as the basic restriction. We also examine the planar (ecliptic) solar sail transfer with gravity-assist flybys around planets.",
author = "V. Koblik and E. Polyakhova and L. Sokolov and A. Shmyrov",
year = "2002",
month = jan,
day = "1",
doi = "10.1016/S0273-1177(02)00156-4",
language = "English",
volume = "29",
pages = "2083--2088",
journal = "Advances in Space Research",
issn = "0273-1177",
publisher = "Elsevier",
number = "12",

}

RIS

TY - JOUR

T1 - Controlled solar sail transfers into the near-sun orbits

AU - Koblik, V.

AU - Polyakhova, E.

AU - Sokolov, L.

AU - Shmyrov, A.

PY - 2002/1/1

Y1 - 2002/1/1

N2 - We present results of numerical simulations of trajectories of a space probe with a flat solar sail which moves from a circular Earth orbit to near-Sun regions. We consider the upper limit of the sail temperature as the basic restriction. We also examine the planar (ecliptic) solar sail transfer with gravity-assist flybys around planets.

AB - We present results of numerical simulations of trajectories of a space probe with a flat solar sail which moves from a circular Earth orbit to near-Sun regions. We consider the upper limit of the sail temperature as the basic restriction. We also examine the planar (ecliptic) solar sail transfer with gravity-assist flybys around planets.

UR - http://www.scopus.com/inward/record.url?scp=0036600656&partnerID=8YFLogxK

U2 - 10.1016/S0273-1177(02)00156-4

DO - 10.1016/S0273-1177(02)00156-4

M3 - Article

AN - SCOPUS:0036600656

VL - 29

SP - 2083

EP - 2088

JO - Advances in Space Research

JF - Advances in Space Research

SN - 0273-1177

IS - 12

ER -

ID: 36366333