A Neptune Orbiter Concept Using Drag Modulated Aerocaptue (DMA) and the Adaptable, Deployable Entry and Placement Technology (ADEPT)
[摘要] Conceptual Neptune orbiter was designed for the purpose of assessing mission feasibilityBuilt off of the 2017 Pre-Decadal Study, but adapted for drag modulation aerocapture.Science payload includes: Narrow Angle camera, Doppler Imager, Magnetometer, Atmospheric Probe (w/ ASI, Nephelometer, Mass Spectrometer). Baseline concept of operations releases probe prior to orbit insertion, but investigations are ongoing to assess the feasibility of bringing the probe to orbit before release.
[发布日期] 2019-04-23 [发布机构]
[效力级别] [学科分类] 工程和技术（综合）
[关键词] AEROCAPTURE;AERODYNAMIC DRAG;ATMOSPHERIC ENTRY;ATMOSPHERIC SOUNDING;CHEMICAL PROPULSION;DYNAMIC CONTROL;ENVIRONMENTAL MONITORING;LAUNCH VEHICLES;MODULATION;NEPTUNE (PLANET);ORBIT INSERTION;PAYLOADS;SYSTEMS ENGINEERING [时效性]
