How To Build a Lunar Base Part 2: The Mission Plan

ROBERT ZUBRIN

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How To Build a Lunar Base Part 2: The Mission Plan

机译：如何建立月球基地第2部分：任务计划

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The Apollo program used a lunar orbit rendezvous plan to reduce the mass of the overall payload required for each lunar mission. However, the spacecraft used for the Apollo missions all used low-performance hypergolic fuels for their propulsion maneuvers after Trans Lunar Injection, a design choice that increases the value of staging propellant in low lunar orbit. These advantages diminish sharply, however, if higher performing propellants such as liquid oxygen-hydrogen (LOx-hy-drogen) or liquid oxygen-mediane (LOx-methane) are used for propulsion after Trans Lunar Injection.

机译：阿波罗计划采用了月球轨道交会计划，以减少每次月球任务所需的总有效载荷的质量。但是，用于“阿波罗”飞行任务的航天器在“越月”注入之后的推进演习中都使用了低性能的高倍燃料，这种设计选择增加了在低月轨道上进行分级推进剂的价值。但是，如果在跨月球注入后使用更高性能的推进剂（例如液氧-氢（LOx-氢）或液氧-中位数（LOx-甲烷））进行推进，这些优势将急剧减少。

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《Space news》 |2005年第8期|p.19-20|共2页
作者
ROBERT ZUBRIN;
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Mars Society;

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正文语种 eng
中图分类航空、航天;
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How To Build a Lunar Base Part 2: The Mission Plan

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