講演情報
[PPS01-P07]Small Next-generation Atmospheric Probe (SNAP) 小型大気突入プローブによる天王星・海王星の将来探査構想
*Sayanagi Kunio1、Dillman Robert2、Atkinson David3、Li Jing8、Saikia Sarag4、Simon Amy5、Spilker Thomas6、Wong Michael7、Hope Drew2、Arora Archit4、Bowen Steven2、Bowes Angela2、Goggin David2、Steven Horan2、Infeld Samantha2、Lecky John2、Marvel Timothy2、McCabe Ryan2、Parikh Anish2、Peterson David2、Primeaux Stephanie2、Scammell Alexander2、Somervill Kevin2、Taylor Lawrence2、Thames Christopher2、Tosoc Hernani2、Tran Loc2 (1.Hampton University、2.NASA Langley Research Center、3.Jet Propulsion Laboratory, California Institute of Technology、4.Purdue University、5.NASA Goddard Space Flight Center、6.Planetary Mission Architect、7.University of California, Berkeley、8.NASA Ames Resaerch Center)
キーワード：
天王星、海王星、大気、惑星探査
We present a concept for a small, atmospheric probe that could be flexibly added to future missions that orbit or fly-by a giant planet as a secondary payload, which we call the Small Next-generation Atmospheric Probe (SNAP). SNAP’s main scientific objectives are to determine the vertical distribution of clouds and cloud-forming chemical species, thermal stratification, and wind speed as a function of depth. As a case study, we present the advantages, cost and risk of adding SNAP to the future Uranus Orbiter and Probe flagship mission; in combination with the mission’s main probe, SNAP would perform atmospheric in-situ measurements at a second location, and thus enable and enhance the scientific objectives recommended by the 2013 Planetary Science Decadal Survey and the 2014 NASA Science Plan to determine atmospheric spatial variabilities.
We envision that the science objectives can be achieved with a 30-kg entry probe ~0.5m in diameter (less than half the size of the Galileo probe) that reaches 5-bar pressure-altitude and returns data to Earth via the carrier spacecraft. As the baseline instruments, the probe will carry an Atmospheric Structure Instrument (ASI) that measures the temperature, pressure and acceleration, a carbon nanotube-based NanoChem atmospheric composition sensor, and an Ultra-Stable Oscillator (USO) to conduct a Doppler Wind Experiment (DWE). We also catalog promising technologies currently under development that will strengthen small atmospheric entry probe missions in the future. While SNAP is applicable to multiple planets, we examine the feasibility, benefits and impacts of adding SNAP to the Uranus Orbiter and Probe flagship mission.
We envision that the science objectives can be achieved with a 30-kg entry probe ~0.5m in diameter (less than half the size of the Galileo probe) that reaches 5-bar pressure-altitude and returns data to Earth via the carrier spacecraft. As the baseline instruments, the probe will carry an Atmospheric Structure Instrument (ASI) that measures the temperature, pressure and acceleration, a carbon nanotube-based NanoChem atmospheric composition sensor, and an Ultra-Stable Oscillator (USO) to conduct a Doppler Wind Experiment (DWE). We also catalog promising technologies currently under development that will strengthen small atmospheric entry probe missions in the future. While SNAP is applicable to multiple planets, we examine the feasibility, benefits and impacts of adding SNAP to the Uranus Orbiter and Probe flagship mission.