Europa Lander Science Definition Team Update
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1 Europa Lander Science Definition Team Update OPAG August 11, 2016 Kevin Hand (JPL), Alison Murray (DRI/UNR), Jim Garvin (GSFC)
2 Science Definition Team Co-Chairs: Alison Murray, DRI/Univ. NV Reno, Jim Garvin, GSFC; Kevin Hand, JPL Ken Edgett, MSSS Bethany Ehlmann, Caltech Jonathan Lunine, Cornell Alyssa Rhoden, ASU Will Brinkerhoff, GSFC Alexis Templeton, CU Boulder Michael Russell, JPL Tori Hoehler, NASA Ames Ken Nealson, USC Sarah Horst, JHU Peter Willis, JPL Alex Hayes, Cornell Brent Christner, Univ FL Chris German, WHOI Aileen Yingst, PSI David Smith, MIT Chris Paranicas, APL Britney Schmidt, GA Tech Planetary scientists, Microbiologists, Geochemists 2
3 Science Definition Team SDT Charter with mission goals defined: Search for evidence of biomarkers and/or signs of extant life. Assess the habitability (particularly through quantitative compositional measurements) of Europa via in situ techniques uniquely available by means of a landed mission. Characterize surface properties at the scale of the lander to support future exploration. 3
4 Science Definition Team Key mission parameters: Lander will be launched on a separate mission. Target launch: 2024 on a SLS. Mission carries its own communication relay (Clipper can only be used as a backup). Battery powered mission: 20 day surface lifetime. Spacecraft dry mass on surface is approximately 350 kg with 35 kg allocation for science payload. Threshold includes chemical analyses of 3 samples from 10 cm depth or deeper. 4
5 Payload Resource Allocations Europa Lander Payload Mass (kg) 35.0 kg (26.6 kg with 32% margin) Current Volume (cm3) (MEV) Total Energy per Mission* (W-hr) (CBE) Total Data Volume per Mission* (Mbits) (CBE) cm
6 Science Trace Matrix (Draft) Goal 1: Search for Evidence of Life on Europa Investigation 1: Detect and characterize any organic indicators of past or present life. Investigation 2: Identify and characterize morphological and textural indicators of life. Investigation 3: Detect and characterize any inorganic indicators of past or present life. Investigation 4: Determine the provenance of sampled material. Investigation 5: Determine if living organisms persist in sampled material [Not part of Threshold]. 6
7 Science Trace Matrix (Draft) Goal 2: Assess the habitability of Europa via in situ techniques uniquely available to a lander mission. Investigation 1: Characterize the non-ice composition of Europa's near-surface material and determine whether there are indicators of chemical disequillibirum and other components essential for life. Investigation 2: Determine the proximity to liquid water at the lander's location. Investigation 3: Detect whether Europa is active today and characterize any observable surface exchange processes to support sample context. 7
8 Science Trace Matrix (Draft) Goal 3: Characterize surface properties at the scale of the lander to support future exploration. Investigation 1: Characterize the biosignature preservation potential (BPP) of accessible surface materials at the landing site. Investigation 2: Characterize the surface dynamics of Europa at the landing site in all three dimensions. Investigation 3: Characterize the material properties of Europa at the landing site. 8
9 Questions? 8/17/16 9
10 Backup 8/17/16 10
11 Schedule Project Weekly telecons, Webex sessions, Working group mtgs Jun 1: SDT Kickoff STM discussions, deliberations; draft, refine Jun 21-22: SDT Co-chairs mtg Report TOC discussed, writing assigned Jul 12-13: SDT F2F Aug 19: Project Report (PPT) Engineering matrix frozen Program STM frozen Report draft #1 compiled Graphics, tables, Etc. compiled Sep 2: Program PPT/Report draft delivered for comment Sep 30: Program Office Report (PPT+3 pages) Glossy Report final draft formatted, indexed, and compiled Nov 30: Glossy delivered11
12 Spacecraft MPV Mass Stackup FS Reserve Mass Deorbit Vehicle (DOV) (aka, the Lander Stack) Powered Descent Vehicle (PDV) + Cruise Vehicle (CV) + Carrier and Orbit Stage (COS) + Descent Stage (DS) Deorbit Stage (DOS) + Lander 350 kg Total FS Dry Mass: 4400 kg Total FS Prop Mass: 8200 kg 5/12/
13 Payload Envelopes 13
14 Lander in Sampling Configuration Arm Workspace 14
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