1. Getting the most out of planetary entry probes Paul Withers Boston University (withers@bu.edu) Planetary Science Seminar, Earth and Atmospheric Sciences, Georgia Tech Monday 2012.02.20 12:00-13:00 1/26Preamble TypicalSmoothing No data

2. What is an entry probe? 2/26 Science issuesEngineering issues Preamble TypicalSmoothing No data

3. 3/26 Related aerospace activities Preamble TypicalSmoothing No data

4. The plan for today Typical trajectory and atmospheric structure reconstruction Creative smoothing of data Creative use of no data Creative use of additional data Preamble TypicalSmoothing No data4/26

5. Where are we? dr/dt = v dv/dt = a-aero + g(r) r0, v0 known Aerodynamic accelerations measured with respect to spacecraft structure Which way is spacecraft pointing? Which way is up? 5/26Preamble TypicalSmoothing No data

6. Pathfinder - Acceleration 6/26Preamble TypicalSmoothing No data

7. Pathfinder altitude profile 7/26Preamble TypicalSmoothing No data

8. Pathfinder speed profile 8/26Preamble TypicalSmoothing No data

9. Density from deceleration Force = m a rho A v 2 = m a Define “C” by rho A v 2 (C/2) = m a 9/26Preamble TypicalSmoothing No data

10. Atmospheric conditions dp/dz = rho g –Find p(z) from rho(z) and an upper boundary p = rho k-Boltzmann T / (molecular mass) –Find T(z) from rho(z) and p(z) and assumed molecular mass How important is precise C for drag? 10/26Preamble TypicalSmoothing No data

11. Pathfinder density 11/26Preamble TypicalSmoothing No data

12. Pathfinder pressure 12/26Preamble TypicalSmoothing No data

13. Pathfinder temperature 13/26Preamble TypicalSmoothing No data

14. Unsmoothed Phoenix data 14/26Preamble TypicalSmoothing No data

15. Which smoothing interval? 15/26Preamble TypicalSmoothing No data

16. Exponential acceleration helps 16/26 We know the acceleration varies like this Acceleration at t=0 is a0 Mean acceleration from –tx to tx is not a0 Mean accelerations over two related time intervals are related - tL = 2 tS We know aL, aS, tS – Find tau! Preamble TypicalSmoothing No data

17. Vary smoothing interval OK! 17/26Preamble TypicalSmoothing No data

18. Smoothed Phoenix data 18/26Preamble TypicalSmoothing No data

19. What if… 19/26Preamble TypicalSmoothing No data

20. Radio link is helpful 20/26Preamble TypicalSmoothing No data

21. How is it helpful? Doppler shift provides line of sight speed One dimensional only! Assumption – All aerodynamic forces are parallel to velocity vector Drag only, no lift Just enough information to solve trajectory 21/26Preamble TypicalSmoothing No data

22. Opportunity accelerations 22/26Preamble TypicalSmoothing No data

23. Opportunity altitudes 23/26Preamble TypicalSmoothing No data

24. Opportunity temperatures 24/26Preamble TypicalSmoothing No data

25. Atmospheric composition molecular mass = dp/dz k T / (rho g) molecular mass = dp/dt k T / (rho g v) 25/26 Easy to measure p, T directly at subsonic speeds on parachute Combine with trajectory information to find atmospheric molecular mass This means composition! Who needs a mass spectrometer? Preamble TypicalSmoothing No data Huygens at Titan N2 atmosphere with some CH4

26. Conclusions Entry probes are not simply engineering making science possible Engineering analysis produces science Imagination is helpful –Situation-specific smoothing approach –Doppler data survives crash landings –Composition can usually be found as well 26/26Preamble TypicalSmoothing No data