in launching (10a) a first orbiter spacecraft (1) from the Earth on a first interplanetary trajectory (31, 33) towards a target planet to be explored,in launching (10b) a second orbiter spacecraft (2) from the Earth on a second interplanetary trajectory (32, 34) towards a rendezvous spot (38), the second interplanetary trajectory not comprising any phase of placing in orbit around the target planet,in recovering a load to be transported and in loading it onto the first orbiter spacecraft (1),in returning the first orbiter spacecraft (1) and the load from the target planet to the rendezvous spot (38),in effecting a docking (14) of the two orbiter spacecraft (1, 2),in returning at least the second orbiter spacecraft (2) and the load, from the rendezvous spot (38) to a terrestrial orbit (41)."/> Method for Lightening the Weight of Fuel Stowed Onboard During an Interplanetary Mission
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Method for Lightening the Weight of Fuel Stowed Onboard During an Interplanetary Mission

机译:减轻行星际飞行中机载燃料重量的方法

摘要

The method for lightening the weight of fuel stowed onboard during an interplanetary mission is characterized in that it consists:in launching (10a) a first orbiter spacecraft (1) from the Earth on a first interplanetary trajectory (31, 33) towards a target planet to be explored,in launching (10b) a second orbiter spacecraft (2) from the Earth on a second interplanetary trajectory (32, 34) towards a rendezvous spot (38), the second interplanetary trajectory not comprising any phase of placing in orbit around the target planet,in recovering a load to be transported and in loading it onto the first orbiter spacecraft (1),in returning the first orbiter spacecraft (1) and the load from the target planet to the rendezvous spot (38),in effecting a docking (14) of the two orbiter spacecraft (1, 2),in returning at least the second orbiter spacecraft (2) and the load, from the rendezvous spot (38) to a terrestrial orbit (41).
机译:一种减轻行星际飞行过程中装载的燃料重量的方法,其特征在于: 在第一行星际轨道( 10 a )从地球发射第一颗轨道飞行器( 1 )时B> 31、33 )指向要探索的目标行星, 在发射( 10 b )从地球以第二行星际轨道( 32、34 )向会合点( 38)发射第二颗轨道飞行器( 2 ),第二个行星际轨迹不包含放置在目标行星周围的轨道上的任何阶段。 在将其加载到第一颗轨道飞行器( 1 )上时, 返回第一颗轨道飞行器( 1 < / B>)和目标行星到集合点的载荷点( 38 ), 影响两个轨道飞行器的对接( 14 ) ( 1、2 ), ,至少返回第二颗轨道飞行器( 2 )和载荷,从会合点( 38 )到地面轨道( 41 )。

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