Trajectory Optimization : For a Mission to the Solar Bow Shock and Minor Planets
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Bester Preis: 93,89 (vom 02.06.2019)
1
Rody Oldenhuis

Trajectory Optimization : For a Mission to the Solar Bow Shock and Minor Planets (2019)

Lieferung erfolgt aus/von: Deutschland ~EN PB NW

ISBN: 9783330073418 bzw. 3330073411, vermutlich in Englisch, LAP Lambert Academic Publishing Mai 2019, Taschenbuch, neu.

Lieferung aus: Deutschland, Versandkostenfrei.
Von Händler/Antiquariat, AHA-BUCH GmbH [51283250], Einbeck, Germany.
Neuware - In November 2003 the Voyager 1 spacecraft pierced through the Solar system's termination shock, followed by Voyager 2 in August 2007. These events marked the beginning of interstellar exploration by spacecraft, which caused a wave of renewed interest in the outer heliosphere throughout the scientific community. This book research investigated the feasibility of a mission to the Solar bow shock (the true interstellar boundary) at -200 AU from the Sun; twice as far as the Voyager spacecraft. The techniques used in designing its trajectory were standard gravitational-assist manoeuvres and/or a single close-proximity flyby with the Sun, and both low-thrust and high-thrust propulsion systems were investigated. Minimum time of flight and maximum spacecraft dry mass were primary objectives, whereas the number and quality of minor planet flybys were secondary objectives. A maximum on the time of flight of 15 years was upheld, extendable to a maximum of 25 years in case the first constraint could not be met or proved overly beneficial to the other objectives. 380 pp. Englisch.
2
Rody Oldenhuis

Trajectory Optimization - For a Mission to the Solar Bow Shock and Minor Planets (2007)

Lieferung erfolgt aus/von: Deutschland ~EN PB NW

ISBN: 9783330073418 bzw. 3330073411, vermutlich in Englisch, LAP Lambert Academic Publishing, Taschenbuch, neu.

Lieferung aus: Deutschland, Versandkostenfrei.
Trajectory Optimization: In November 2003 the Voyager 1 spacecraft pierced through the Solar system`s termination shock, followed by Voyager 2 in August 2007. These events marked the beginning of interstellar exploration by spacecraft, which caused a wave of renewed interest in the outer heliosphere throughout the scientific community. This book research investigated the feasibility of a mission to the Solar bow shock (the true interstellar boundary) at -200 AU from the Sun twice as far as the Voyager spacecraft. The techniques used in designing its trajectory were standard gravitational-assist manoeuvres and/or a single close-proximity flyby with the Sun, and both low-thrust and high-thrust propulsion systems were investigated. Minimum time of flight and maximum spacecraft dry mass were primary objectives, whereas the number and quality of minor planet flybys were secondary objectives. A maximum on the time of flight of 15 years was upheld, extendable to a maximum of 25 years in case the first constraint could not be met or proved overly beneficial to the other objectives. Englisch, Taschenbuch.
3
9783330073418 - Oldenhuis, Rody: Trajectory Optimization - For a Mission to the Solar Bow Shock and Minor Planets
Oldenhuis, Rody

Trajectory Optimization - For a Mission to the Solar Bow Shock and Minor Planets (2019)

Lieferung erfolgt aus/von: Deutschland ~EN PB NW

ISBN: 9783330073418 bzw. 3330073411, vermutlich in Englisch, 380 Seiten, LAP Lambert Academic Publishing, Taschenbuch, neu.

Lieferung aus: Deutschland, Versandkosten nach: Deutschland, Versandkostenfrei.
Von Händler/Antiquariat, Syndikat Buchdienst, [4235284].
In November 2003 the Voyager 1 spacecraft pierced through the Solar system's termination shock, followed by Voyager 2 in August 2007. These events marked the beginning of interstellar exploration by spacecraft, which caused a wave of renewed interest in the outer heliosphere throughout the scientific community. This book research investigated the feasibility of a mission to the Solar bow shock (the true interstellar boundary) at -200 AU from the Sun twice as far as the Voyager spacecraft. The techniques used in designing its trajectory were standard gravitational-assist manoeuvres and/or a single close-proximity flyby with the Sun, and both low-thrust and high-thrust propulsion systems were investigated. Minimum time of flight and maximum spacecraft dry mass were primary objectives, whereas the number and quality of minor planet flybys were secondary objectives. A maximum on the time of flight of 15 years was upheld, extendable to a maximum of 25 years in case the first constraint could not be met or proved overly beneficial to the other objectives. 2019, Taschenbuch / Paperback, Neuware, H: 220mm, B: 150mm, T: 22mm, 584g, 380, Internationaler Versand, Selbstabholung und Barzahlung, PayPal, offene Rechnung, Banküberweisung.
4
Rody Oldenhuis

Trajectory Optimization: For a Mission to the Solar Bow Shock and Minor Planets (2019)

Lieferung erfolgt aus/von: Deutschland EN PB NW

ISBN: 9783330073418 bzw. 3330073411, in Englisch, 380 Seiten, LAP Lambert Academic Publishing, Taschenbuch, neu.

Lieferung aus: Deutschland, Gewöhnlich versandfertig in 24 Stunden, Versandkostenfrei. Tatsächliche Versandkosten können abweichen.
Von Händler/Antiquariat, averdo24.
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