| 翻訳と辞書 |
Minotaur V
}}
The Minotaur V is an American expendable launch system derived from the Minotaur IV, itself a derivative of the LGM-118 Peacekeeper ICBM. It was developed by Orbital Sciences Corporation, and made its maiden flight on 7 September 2013 carrying the Lunar Atmosphere and Dust Environment Explorer spacecraft for NASA.〔(【引用サイトリンク】title=Lunar Atmosphere and Dust Environment Explorer (LADEE) Mission website )〕
==Design==
The Minotaur V is a five-stage vehicle, and is designed to place up to of payload into a geosynchronous transfer orbit, or on a trans-lunar trajectory. It consists of a Minotaur IV+, with a Star-37 as a fifth stage. Two variants are available, one with a spin-stabilized Star-37FM upper stage, and the other with a Star-37FMV capable of three-axis stabilization.〔 The Star-37FMV upper stage is heavier, reducing payload capacity, but is more maneuverable.
抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』
■ウィキペディアで「Minotaur V」の詳細全文を読む
スポンサード リンク
| 翻訳と辞書 : 翻訳のためのインターネットリソース |
Copyright(C) kotoba.ne.jp 1997-2016. All Rights Reserved.
|
|