Name: Interplanetary Mission Design Handbook: Earth-to-Mars Mission Opportunities and Mars-to-Earth Return Opportunities 2009-2024 (en Inglés)
Price: 40.15 USD
Availability: InStock
Author: Administration, National Aeronautics and
ISBN: 9781503059344

portada Interplanetary Mission Design Handbook: Earth-to-Mars Mission Opportunities and Mars-to-Earth Return Opportunities 2009-2024 (en Inglés)

Interplanetary Mission Design Handbook: Earth-to-Mars Mission Opportunities and Mars-to-Earth Return Opportunities 2009-2024 (en Inglés)

Formato

Libro Físico

Autor

National Aeronautics and Administration

Editorial

Createspace

Idioma

Inglés

N° páginas

164

Encuadernación

Tapa Blanda

Dimensiones

28.0 x 21.6 x 0.9 cm

Peso

0.39 kg.

ISBN13

9781503059344

Categorías

Ciencia espacial

Interplanetary Mission Design Handbook: Earth-to-Mars Mission Opportunities and Mars-to-Earth Return Opportunities 2009-2024 (en Inglés)

National Aeronautics and Administration (Autor) · Createspace · Tapa Blanda

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Reseña del libro "Interplanetary Mission Design Handbook: Earth-to-Mars Mission Opportunities and Mars-to-Earth Return Opportunities 2009-2024 (en Inglés)"

This handbook provides information for trajectory designers and mission planners to determine Earth-Mars and Mars-Earth mission opportunities for the years 2009-2024. These studies were performed in support of a human Mars mission scenario that will consist of two cargo launches followed by a piloted mission during the next opportunity approximately 2 years later. "Porkchop" plots defining all of these mission opportunities are provided which include departure energy, departure excess speed, departure declination arrival excess speed, and arrival declinations for the mission space surrounding each opportunity. These plots are intended to be directly applicable for the human Mars mission scenario described briefly herein. In addition, specific trajectories and several alternate trajectories are recommended for each cargo and piloted opportunity. Finally, additional studies were performed to evaluate the effect of various thrust-to-weight ratios on gravity losses and total time-of-flight tradeoff, and the resultant propellant savings and are briefly summarized.