Sensor Systems of the NASA Airborne Science Program

The National Aeronautics and Space Administration maintains a variety of aircraft and sensor systems dedicated to the support of remote sensing research. Two Lockheed ER-2s (S-model U-2,) a DC-8, and several U.S. Dept. of Energy aircraft provide multi-level platforms for both NASA and investigator-owned sensors. Data are collected for the atmospheric, land, and ocean processes aspects of the NASA Earth Science program, as well as for universities and other government agencies. Several of these systems are being used to validate algorithms for the NASA Earth Observing System. 

The NASA aircraft, located at Dryden Flight Research Center, are used as test-beds for advanced sensor design and satellite simulation, as well as to support scientific and operational data collection campaigns. Numerous sensor systems are in use and under development by NASA, including multispectral imaging devices, a SAR system, and a suite of large-format mapping cameras. All instruments are spectrally, spatially, and radiometrically calibrated on a routine basis. The aircraft themselves are equipped with navigation systems that continuously record GPS location and platform attitude data. 

The systems described here are facility NASA sensors, and are generally available to the science community; they reside at either Ames Research Center or the Jet Propulsion Laboratory (noted as ARC or JPL, respectively.) There are a variety of other sensors that fly on these aircraft that are owned by individual investigators, which are not within the scope of this document. 

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AVIRIS.jpg
AVIRIS Insturument undergoing pre-flight checks
AVIRIS Imagery of Mt. St. Helens
AVIRIS Image of Mount St. Helens

AVIRIS (Airborne Visible and Infrared Imaging Spectrometer - JPL)

The AVIRIS is the second in a series of imaging spectrometer instruments developed at the Jet Propulsion Laboratory (JPL) for earth remote sensing. This instrument uses scanning optics and four spectrometers to image a 614 pixel swath simultaneously in 224 contiguous spectral bands. 

AVIRIS parameters are as follows:

  • IFOV: 1 mrad
  • Ground Resolution: 66 feet (20 meters) at 65,000 feet
  • Total Scan Angle: 30 degrees
  • Swath Width: 5.7 nmi (10.6 km) at 65,000 feet
  • Digitization: 12-bits
Spectrometer
Wavelength
#Bands
Bandwidth
1
0.41 - 0.70 µm
31
9.4 nm
2
0.68 - 1.27 µm
63
9.4 nm
3
1.25 - 1.86 µm
63
9.7 nm
4
1.84 - 2.45 µm
63
9.7 nm

Notes: This instrument is flown on the ER-2 aircraft. All data collection missions are coordinated through JPL. 

(See the AVIRIS homepage at http://makalu.jpl.nasa.gov/aviris.html)


MODIS Airborne Simulator

MODIS imagery from the Alaska-April95 Campaign

MODIS imagery from the WINCE Campaign

MODIS imagery of the Arkansas River Gorge, Colorado

MODIS Airborne Simulator (ARC)

The MODIS Airborne Simulator (MAS) is a multispectral scanner configured to approximate the Moderate-Resolution Imaging Spectrometer (MODIS), an instrument to be orbited on the NASA EOS-AM1 platform. MODIS is designed to measure terrestrial and atmospheric processes. The MAS was a joint project of Daedalus Enterprises, Berkeley Camera Engineering, and Ames Research Center. The MODIS Airborne Simulator records fifty spectral bands, configured as follows:
Spectral
Channel
Band Center
(µm)
Bandwidth
(µm)
Spectral Range
1 0.4649 0.0397 0.4451-0.4848
2 0. 5494 0.0417 0.5285-0.5703
3 0.6550 0.0511 0.6294-0.6805
4 0.7024 0.0415 0.6816-0.7231
5 0.7431 0.0420 0.7221-0.7641
6 0.8248 0.0427 0.8034-0.8461
7 0.8667 0.0414 0.8460-0.8874
8 0.9072 0.0409 0.8867-0.9276
9 0.9476 0.0397 0.9277-0.9674
10 1.6422 0.0519 1.6163-1.6682
11 1.6975 0.0505 1.6722-1.7228
12 1.7499 0.0506 1.7245-1.7752
13 1.8014 0.0491 1.7768-1.8259
14 1.8548 0.0489 1.8303-1.8792
15 1.9044 0.0487 1.8801-1.9288
16 1.9553 0.0483 1.9312-1.9794
17 2.0048 0.0487 1.9804-2.0291
18 2.0551 0.0484 2.0309-2.0793
19 2.1037 0.0486 2.0794-2.1280
20 2.1532 0.0483 2.1291-2.1774
21 2.2019 0.0481 2.1779-2.2259
22 2.2522 0.0486 2.2278-2.2675
23 2.3021 0.0487 2.2777-2.3265
24 2.3512 0.0476 2.3274-2.3750
25 2.4005 0.0483 2.3764-2.4246
26 3.1192 0.1616 3.0384-3.2000
27 3.2809 0.1486 3.2066-3.3552
28 3.4330 0.1617 3.3521-3.5138
29 3.5940 0.1539 3.5170-3.6709
30 3.7449 0.1449 3.6724-3.8174
31 3.9069 0.1602 3.8267-3.9870
32 4.0707 0.1554 3.9929-4.1484
33 4.1699 0.0669 4.1365-4.2034
34 4.4029 0.1255 4.3401-4.4656
35 4.5404 0.1512 4.4648-4.6160
36 4.6979 0.1591 4.6184-4.7775
37 4.8536 0.1516 4.7778-4.9294
38 5.0033 0.1468 4.9298-5.0767
39 5.1588 0.1400 5.0888-5.2288
40 5.3075 0.1327 5.2412-5.3738
41 5.3977 0.0755 5.3590-5.4365
42 8.5366 0.3950 8.3391-8.7341
43 9.7224 0.5365 9.4541-9.9906
44 10.5071 0.4579 10.278-10.736
45 11.0119 0.4710 10.776-11.247
46 11.9863 0.4196 11.776-12.196
47 12.9013 0.3763 12.713-13.089
48 13.2702 0.4584 13.041-13.500
49 13.8075 0.5347 13.540-14.075
50 14.2395 0.3775 14.051-14.428
Sensor/Aircraft Parameters:
  • Spectral Bands: 50 (16-bit resolution)
  • IFOV: 2.5 mrad
  • Ground Resolution: 163 feet (50 meters at 65,000 feet)
  • Swath Width: 19.9 nmi (36 km)
  • Total Scan Angle: 85.92 degrees
  • Pixels/Scan Line: 716
  • Scan Rate: 6.25 Hz
  • Ground Speed: 400 kts (206 m/second)
  • Roll Correction: Plus or minus 3.5 degrees (approx.)
See the webpage http://mas.arc.nasa.gov

MASTER instrument in the calibration lab

MASTER (MODIS/ASTER Airborne Simulator - ARC)

The MASTER is similar to the MAS, with the thermal bands modified to more closely match the NASA EOS ASTER (Advanced Spaceborne Thermal Emission and Reflection Radiometer) satellite instrument, which is scheduled for launch in 1998. It is intended primarily to study geologic and other Earth surface properties. Flying on both high and low altitude aircraft, the MASTER will be operational in early 1998. Its fifty spectral bands are configured as follows:
Spectral
Channel
Band Center
(µm)
Bandwidth
(µm)
Spectral Range
1 0.460 0.04 0.440-0.480
2 0.500 0.04 0.480-0.520
3 0.540 0.04 0.520-0.560
4 0.580 0.04 0.560-0.600
5 0.660 0.06 0.630-0.690
6 0.710 0.04 0.690-0.730
7 0.750 0.04 0.730-0.770
8 0.800 0.04 0.780-0.820
9 0.865 0.04 0.845-0.885
10 0.905 0.04 0.885-0.925
11 0.945 0.04 0.925-0.965
12 1.625 0.05 1.600-1.650
13 1.675 0.05 1.650-1.700
14 1.725 0.05 1.700-1.750
15 1.775 0.05 1.750-1.800
16 1.825 0.05 1.800-1.850
17 1.875 0.05 1.850-1.900
18 1.925 0.05 1.900-1.950
19 1.975 0.05 1.950-2.000
20 2.075 0.05 2.050-2.100
21 2.160 0.05 2.135-2.185
22 2.210 0.05 2.185-2.235
23 2.260 0.05 2.235-2.285
24 2.3295 0.065 2.297-2.362
25 2.3945 0.065 2.362-2.427
26 3.150 0.15 3.075-3.225
27 3.300 0.15 3.225-3.375
28 3.450 0.15 3.375-3.525
29 3.600 0.15 3.525-3.675
30 3.750 0.15 3.675-3.825
31 3.900 0.15 3.825-3.975
32 4.050 0.15 3.975-4.125
33 4.200 0.15 4.125-4.275
34 4.375 0.15 4.300-4.450
35 4.500 0.15 4.425-4.575
36 4.650 0.15 4.575-4.725
37 4.800 0.15 4.725-4.875
38 4.950 0.15 4.875-5.025
39 5.100 0.15 5.025-5.175
40 5.250 0.15 5.175-5.325
41 7.900 0.4 7.70-8.10
42 8.300 0.4 8.10-8.50
43 8.700 0.4 8.50-8.90
44 9.100 0.4 8.90-9.30
45 9.700 0.4 9.50-9.90
46 10.100 0.4 9.90-10.30
47 10.625 0.65 10.30-10.95
48 11.300 0.7 10.95-11.65
49 12.050 0.5 11.80-12.30
50 12.750 0.5 12.50-13.00
Sensor/Aircraft Parameters:
  • Spectral Bands: 50 (16-bit resolution)
  • IFOV: 2.5 mrad
  • Ground Resolution: 12-50 meters (variable w/ altitude)
  • Total FOV: 85.92 degrees
  • Pixels/Scanline: 716
  • Scan Rate: 6.25 - 25 Hz
(See the homepage at http://masterweb.jpl.nasa.gov)
MISR instrument
A cut-away view of the MISR instrument

AirMISR (Airborne Multi-angle Imaging SpectroRadiometer - JPL)

This is an airborne instrument for obtaining multi-angle imagery similar to that of the satellite-borne MISR instrument, which is designed to contribute to studies of the Earth's ecology and climate. AirMISR flies on the NASA-owned ER-2 aircraft. It was built for NASA by the Jet Propulsion Laboratory in Pasadena, California. 

(See the homepage at http://www-misr.jpl.nasa.gov/armain.html)

Misoula, Montana
AIRSAR image of Missoula Mt.

AIRSAR (Airborne Synthetic Aperture Radar - JPL)

This is an experimental system managed by the NASA Jet Propulsion Laboratory (JPL,) that flies on the DC-8 aircraft. It simultaneously acquires data in the L, P, and C-Bands in multiple polarizations.
The system was designed in support of the Space Shuttle Imaging Radar-C (SIR-C) program, but is widely used in the SAR remote sensing research community. 

(See the homepage at http://southport.jpl.nasa.gov/desc/AIRSdesc.html)


TMS mounted in the Q-Bay

TMS (Thematic Mapper Simulator - ARC)

This is a Daedalus AADS-1268 scanner that flies on the ER-2 aircraft and simulates the LANDSAT TM instrument, with slightly higher spatial resolution, and several extra bands.
Band
Wavelength µm
1 0.42- 0.45
2 (TM1) 0.45- 0.52
3 (TM2) 0.52- 0.60
4 0.60- 0.62
5 (TM3) 0.63- 0.69
6 0.69- 0.75
7 (TM4) 0.76- 0.90
8 0.91- 1.05
9 (TM5) 1.55- 1.75
10 (TM7) 2.08- 2.35
11 (TM6) High Gain 8.5- 14.0
12 (TM6) Low Gain 8.5- 14.0
  • Spatial Resolution: 25 meters (all bands) from 19.8 km (65,000 ft.)
  • Total Field of View: 42.5 degrees
  • IFOV: 1.25 mrad
Notes: All bands are 8-bit digitization; onboard blackbody sources are carried for thermal calibration.
The system is scheduled to be upgraded to 16-bit resolution in late 1998. 

(See the homepage at http://asapdata.arc.nasa.gov/Sensors.htm)


AOCI image of the Missippi Delta

AOCI (Airborne Ocean Color Imager - ARC)

The AOCI is a high altitude multispectral scanner built by Daedalus Enterprises, designed for oceanographic remote sensing. It provides 10-bit digitization of eight bands in the visible/near-infrared region of the spectrum, plus two 8-bit bands in the near and thermal infrared. The bandwidths are as follows:
Channel
Wavelength, µm
Digitization
1
0.436 - 0.455
10 bit
2
0.481 - 0.501
10 bit
3
0.511 - 0.531
10 bit
4
0.554 - 0.575
10 bit
5
0.610 - 0.631
10 bit
6
0.655 - 0.676
10 bit
7
0.741 - 0.800
10 bit
8
0.831 - 0.897
10 bit
9
0.989 - 1.054
8 bit
10
8.423 - 12.279
8 bit
  • Spatial Resolution: 50 Meters from 19.8 km (65,000 ft.)
  • Total Field of View: 85 degrees
  • IFOV: 2.5 mrad
Note: The system is scheduled to be upgraded to 16-bit resolution in late 1998. 

(See the homepage at http://asapdata.arc.nasa.gov/Sensors.htm)


MAMS composites

MAMS Catalina Island Composite

MAMS (Multispectral Atmospheric Mapping Sensor - ARC)

The MAMS is a modified Daedalus Scanner flown aboard the ER-2 aircraft. It is designed to study weather related phenomena including storm system structure, cloud-top temperatures, and upper atmospheric water vapor. The scanner retains the eight silicon-detector channels in the visible/near-infrared region found on the Daedalus Thematic Mapper Simulator, with the addition of four channels in the infrared relating to specific atmospheric features. The spectral bands are as follows:
Channel
Wavelength, µm
1
(LSBs for Channels 9-12)
2
0.45 - 0.52
3
0.52 - 0.60
4
0.57 - 0.67
5
0.60 - 0.73
6
0.65 - 0.83
7
0.72 - 0.99
8
0.83 - 1.05
9
3.55 - 3.93 (6.20- 6.90 optional)
10
3.55 - 3.93 (6.20- 6.90 optional)
11
10.3 - 12.1
12
12.5 - 12.8
  • Spatial Resolution: 50 or 100 meters from 19.8 km (65,000 ft.)
  • Total Field of View: 85.92 degrees
  • IFOV: 2.5 or 5.0 mrad (selectable)
Notes: Channels 9 - 12 are digitized to 10 bits; all others are 8-bit. Blackbody sources are carried for IR calibration. The system is scheduled to be upgraded to 16-bit resolution in late 1998. 

(See the homepage at http://wwwghcc.msfc.nasa.gov/irgrp/mams)


A-4 Configuration (RC-10 and HR-732)

RC-10 Image of San Francisco

Aerial Camera Systems (ARC)

The ER-2 can carry a variety of film camera systems. Several of these cameras are calibrated for precision photogrammetry, and the film may be used to generate digital ortho-photos or high-resolution digital elevation models.
Camera
Type
Lens
Film
Format
Ground
Coverage
Nominal
Resolution
Scale
RC-10
6"/f4
9" X 9"
30 X 30km
3.0-8.0m
1:130,000
RC-10
12"/f4
9" X 9"
15 X 15km
1.5-4.0m
1:65,000
HR-732
24"/f8
9" X 18"
7.4 X 15km
0.6-3.0m
1:32,500
IRIS
(Panoramic)
24"/f3.5
4.5" X 35"
3.7 X 40km
(Nadir)
0.3-2.0m
1:32,500
Note: Spatial parameters are for the ER-2 at 19.8km altitude; actual resolution is a function of target contrast. Missions are typically flown with 60% forward frame overlap for stereo coverage. RC-30 cameras are also available on the Dept. of Energy aircraft. 

(See the homepage at http://asapdata.arc.nasa.gov/Sensors.htm)

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