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The Value of Enhanced Delta V Capacity: a Europa Clipper Case Study

机译:增强型Delta V容量的价值:欧罗巴剪裁案例研究

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Interplanetary flight can take years due to the vast distances, but the time spent traveling those distances is related to the amount of velocity change (also known as delta-v) rockets can provide. The Europa Clipper mission is analyzed to gain some insight into the value of a mission architecture's velocity change capacity. Value models considering time, cost, spacecraft, space mission operations, and return capability are used to rank preference for Venus-Earth-Earth-Gravity-Assist or Direct to Jupiter mission architectures. The analysis shows that the space mission operations costs are insignificant compared to the costs of the spacecraft and launch vehicles, but differences in spacecraft cost entailed by required spacecraft life show the advantages of selecting the Direct to Jupiter architecture. The cost of the Space Launch System required for the Direct architecture is a strong factor in determining which architecture has greater value. The cost of the Atlas V launcher and the spacecraft payload are also relatively strong influences on choice of architecture when mission value is not included in the analysis, so that extending the mission does not impact the architecture selection. However, when mission value is included, the Direct architecture is favored even when the cost of the SLS is much higher than the cost of the Atlas V. The discount rate and value of mission time are stronger influences than the cost of the Atlas V from this perspective and their influence grows as the mission is extended. The cost of the spacecraft and Atlas V became relatively minor factors in the architecture choice when mission value is considered. For the case of Europa Clipper the value of velocity change depends on the relative costs of the more capable launch vehicles regardless of whether mission value is considered. However, mission value seems of central importance, and it is connected to time: the mission is worth more when results are obtained sooner. Even with mission v
机译:行星际航班由于距离距离可能需要数年,但花费这些距离的时间与速度变化(也称为Delta-V)火箭提供的时间有关。分析Europa Clipper Mission以获得一些洞察任务架构的速度变化容量的价值。考虑时间,成本,航天器,空间任务操作和返回能力的价值模型用于对金星 - 地球 - 地球 - 重力辅助或直接到木星任务架构的偏好。该分析表明,与航天器和发动车辆的成本相比,空间任务运营成本是微不足道的,但是所需航天器寿命所需的航天器成本的差异表明了选择直接到木星架构的优势。直接架构所需的空间发射系统的成本是确定哪个架构具有更大价值的强因素。当任务价值未包含在分析中时,ATLAS V启动器和航天器有效载荷的成本也对架构的选择的影响也相对强烈影响,因此扩展任务不会影响架构选择。然而,当包括任务价值时,即使SLS的成本远高于ATLAS V的成本,直接架构也受到青睐。任务时间的折扣率和价值比ATLAS V的成本更强随着使命延长,这种观点和它们的影响力增长。当考虑任务价值时,航天器和阿特拉斯族的成本变得相对较小的因素。对于Europa Clipper的情况,速度变化的值取决于不管考虑任务价值是否更有能力的发动机的相对成本。但是,使命价值似乎是核心重要性,它与时间相连:当结果越早获得时,使命值得更多。即使是任务v

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