NASA Airborne Science Program • Armstrong Flight Research Center

NASA ER-2 Stratospheric Science Mission Simulator

Lockheed ER-2 (U-2 derived) High-Altitude Atmospheric Research Platform (#806 / #809)
ALT: 68,000 FT COL BYPASS: 94.8% SWATH: 37.1 KM

Stratospheric Cross-Section & Aircraft Trajectory

Click or drag aircraft vertically on canvas
ALT: 68,000 FT | STRATOSPHERE | TAS: 410 KTS
Ambient Pressure
48.2 hPa
Standard Sea Level: 1013 hPa
Atmospheric Mass Bypassed
94.8%
Column beneath aircraft
Ambient Temp (Inversion)
-56.5 °C
Stratospheric isothermal/rise
Sensor Swath Width
37.1 km
Nadir Field-of-View 85°
Payload Weight
1,820 lbs
Capacity: 2,600 lbs max
True Airspeed (TAS)
410 kts
Mach 0.71 Cruise

Stratospheric Research Flight Clearance Telemetry

NASA Form AFRC-ER2-SCI
Flight Leg / Checkpoint Altitude Ambient Press. Ozone Density Ground Footprint (GSD) Operational Phase
T+00:45 Climb Pass 35,000 ft 238 hPa 0.04 ppmv 18.8 km (7.1 m GSD) Troposphere Storm Anvil Overflight
T+01:15 Tropopause Transition 52,000 ft 105 hPa 0.28 ppmv 27.9 km (10.5 m GSD) Cold-Point Tropopause Crossing (-68°C)
T+02:30 Cruise Transect 68,000 ft 48.2 hPa 2.45 ppmv 37.1 km (13.7 m GSD) Active Science Data Acquisition (94.8% Column Bypassed)
T+06:00 Decent & Spiral Inbound 25,000 ft 376 hPa 0.02 ppmv 13.4 km (5.1 m GSD) Aerosol Filter Purge & Recovery Descent
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