1. September 07 Airborne Experiment

2. September 07 Experiment P-3 flights from Thule and Kangerdlussuaq 150 MHz and 450 MHz Radars Maximum altitude allowable Experiment Plan Posted at –http://www-bprc.mps.ohio- state.edu/rsl/gismo/documents/GISMO_07.pdf

3. Technical Objectives for September ’07 Experiment 1) Acquire data over the May 2006 flight line to compare high and low altitude observations and to compare interferometry acquired with different baselines. Are results consistent with theory? 2) Acquire data at 150 MHz and 450 MHz along every flight line and compare backscatter and interferometric frequency response? Are the results consistent with theory? 3) Acquire data over areas where we expect to find subglacial water. Is water detectable either from backscatter maps or from topography? 4) Acquire data over regions of increasing surface roughness. This may require observations over heavily crevassed shear margins such as those found around Jacobshavn Glacier. Can we successfully implement interferogram phase filtering? 5) Acquire data for tomographic analysis 6) Investigate repeat pass interferometry over repeat periods of days. 7) Verify volume clutter is weak (all snow zones) 8) Collect data over thick and thin ice to test for absorption effects

4. Update to May 06 Experiment Plan ParameterValue Frequency150 Mhz, 450 MHz Band width20 MHz, 40 MHz Range window Start 4 us to 44 us with pulse 1 (lo-gain) Then 15 us to 55 us pulse 2 (hi-gain) Pulse width3 us PRF10 KHz (5 Khz for each pulse) Baseline offsetReturn flight 25 m south of outbound flight CalibrationRough ocean observations at these specs Aircraft elevation above ellipsoid (geoid)~ 26000 ft (install additional external attunuators into the receiver Antennas configured for two frequenciesRedesigned At least one flight with multiple repeats for tomography Racetrack design High elevation flights on any flights of opportunity26,000 ft Early evaluation of Greenland dataVECO assisted DVD or electronic file transfer to KU after first GISMO flight: Process to depth sounder mode; Process to SAR image

5. Constraints on Flight Operations Fly at maximum allowable altitude Limit flight duration to allow for daily data Q/A and experiment modifications (about 6 hours assuming 150 Gb/hour and 3, 300 Gb disks) Allow enough field time to repeat flight lines Fly over high and low clutter areas Fly over areas where some information on basal properties is known VHF and UHF radars cannot operate simultaneously – repeat P-band and VHF along same track to within 30 m Schedule 2 to 4 repeat flights at 30 m horizontal offsets for tomography

6. Planned Flight Lines

7. Proposed Flight Lines 1.Ice Streams 2.Outlet Glaciers 3.Jacobshavn 4.OSU Clusters

8. Jacobshavn 1.Open Ocean Segment down Sondrestrom Fjord 2.Several passes over Jacobshavn glacier with tomography racetrack 3.Flight over GRIP GISP drill sites 4.Outbound at 26000 ft, Return flight at 500 feet 5.Flights at 150 MHz and 450 MHz

9. Thule 2 Flight of NEMES drilling site location Flights across crevassed areas of outlet glaciers and across grounding lines Tomography racetrack over Mt. Gogineni Segment over open ocean Flight at 150 and 450 MHz

10. Thule Flight 1 Flight 1 –Segment over open ocean –Repeat segment flown at 150 MHz in May 2006 –Flights at 150 and 450 MHz –Overflight of NGRIP and North East Ice Stream

11. Clusters Measurements where 2-dimensional surveys have been conducted: –OSU Clusters –Dye 3 Measurements over East Greenland outlet glaciers

12. Range Window Duration (Clusters) 1500’ elevation over ice sheet26000’ Presssure Altitude

13. Range Window Duration (26000’ Pressure Altitude)

14. Flight Hour Summary Flight line total time (hours)data collection time (hours) Thule 26.65.4 Thule 15.14.8 Sonde7.46.6 Clusters4.14 2 flights per line46.441.6

15. August 07 Test Flights and Transit

16. Test Flights Plan one test flight with at least one contingency flight Data collection to be beyond 200 mile limit Data collection portion of flight to last 2 hours Antennas configured at 450 MHz (operate radar at 450 and 150 by utilizing harmonic)

17. Test Flight Objectives Verify that the radar system reliably transmits/receives/records data at 450 and 150 MHz. Verify and practice operational procedures including procedures for turning on and turning off the radar in concert with aircraft crew manipulation of aircraft power.

18. Test Flight Approach Conduct 1, 2 hour data collection test flight (allow for one contingency flight) Record ocean waveforms and verify consistent, uninterrupted data acquitision. Verify chirp shape and duration. Verify loop sensitivity Verify system bandwidth Verify presum rates Verify GPS data stream link Conduct two +-60 degree rolls to acquire antenna pattern data. Transfer test data to KCJ disk and process data. Label all cables. Calibration Tests????? Test contingency plans (several options in case of a primary radar failure?).

19. Test Flight Success Criteria Radar transmits receives and records uninterrupted data over the designed bandwidths at 150 and 450 MHz. Data are downloadable and processable. Tools necessary for calibration (eg load terminators) are available. Procedure pages are available for the operator and vetted

20. Go/No Go Decisions for Discussion What do we do if we observe intermittent or more serious failures? What do we do if there is another catastrophic failure? Do we address problems in the plane? Do we immediately dismantle and put the radar box on a bench at WFF (adequate room to easily pull radar box)? Do we ship back to Lawrence?

21. Transit Transit to Thule with 450 MHz antennas Do first Thule flight for GISMO to secure some data early Interleave remaining flights with ATM/MCARD on subsequent flights noting that it would be useful to complete 450 MHz flights before changing to 150 MHz antennas Transit to Sonde at 150 MHz Complete ATM/MCARD and 150 MHz GISMO flights Complete 450 MHz GISMO flights Return transit at 450 MHz for additional calibration work