Entri Populer

Minggu, 28 November 2010

Sejarah Satelit Landsat 7

Landsat 7 History

April 15, 1999 - present

Landsat 7
Figure 1. Landsat 7



Landsat 7 
launch
Movie 1. Launch of Landsat 7
Download Small Landsat 7 Launch Movie .mov (23.2 MB)
Download Large Landsat 7 Launch Movie .mov (121 MB)
Download QuickTime Player


Participants
  • NASA
  • National Oceanic and Atmospheric Administration (NOAA) (initial participant)
  • Department of the Interior (DOI) U.S. Geological Survey (USGS)
  • Spacecraft bus: Lockheed Martin Missiles & Space
  • Enhanced Thematic Mapper Plus (ETM+): Hughes Santa Barbara Remote Sensing

Launch
  • Date: April 15, 1999
  • Vehicle: Delta II
  • Launched by: NASA
  • Site: Western Test Range at Vandenberg Air Force Base, California

Figure 2. 
Landsat 7 Figure 2. 
Landsat 7 Figure 2. 
Landsat 7 Figure 2. 
Landsat 7 Figure 2. 
Landsat 7
Figure 2. Landsat 7

Spacecraft
  • Power provided by a single Sun-tracking solar array and two 50 Ampere-Hour (AHr), Nickel Cadmium (NiCd) batteries
  • Attitude control provided through four reaction wheels (pitch, yaw, roll, and skew); three 2-channel gyros with celestial drift updating; a static Earth sensor; a 1750 processor; and torque rods and magnetometers for momentum uploading
  • Orbit control and backup momentum unloading provided through a blow-down monopropellant hydrazine system with a single tank containing 270 pounds of hydrazine, associated plumbing, and twelve 1-pound-thrust jets
  • Weight: approx. 4,800 lbs (2,200 kg)
  • Length: 4.3 m (14 ft)
  • Diameter: 2.8 m (9 ft)

Communications
  • Direct Downlink with Solid State Recorders (SSR)
  • Data rate: 150 Mbps

Orbit
  • Worldwide Reference System-2 (WRS-2) path/row system
  • Sun-synchronous orbit at an altitude of 705 km (438 mi)
  • 233 orbit cycle; covers the entire globe every 16 days (except for the highest polar latitudes)
  • Inclined 98.2° (slightly retrograde)
  • Circles the Earth every 98.9 minutes
  • Equatorial crossing time: 10:00 a.m. +/- 15 minutes

Sensors
Enhanced Thematic Mapper Plus (ETM+)
  • Eight spectral bands, including a pan and thermal band:
    • Band 1 Visible (0.45 – 0.52 µm) 30 m
    • Band 2 Visible (0.52 – 0.60 µm) 30 m
    • Band 3 Visible (0.63 – 0.69 µm) 30 m
    • Band 4 Near-Infrared (0.77 – 0.90 µm) 30 m
    • Band 5 Near-Infrared (1.55 – 1.75 µm) 30 m
    • Band 6 Thermal (10.40 – 12.50 µm) 60 m Low Gain / High Gain
    • Band 7 Mid-Infrared (2.08 – 2.35 µm) 30 m
    • Band 8 Panchromatic (PAN) (0.52 - 0.90 µm) 15 m
  • Ground Sampling Interval (pixel size): 30 m reflective, 60 m thermal
  • Added the Band 6 Low and High gain 60 m thermal bands
  • On-board calibration was added to Landsat 7: a Full Aperture Solar Calibrator (FASC) and a Partial Aperture Solar Calibrator (PASC), in addition to the 2 calibration lamps

Other Characteristics
  • Scene size: 170 km x 185 km (106 mi x 115 mi)
  • Design Life: Minimum of 5 years
Landsat 7
Figure 3. Landsat 7

sumber :
http://landsat.usgs.gov/about_landsat7.php

Sejarah Satelit Landsat 6

Landsat 6 History

October 5, 1993 (did not achieve orbit)



Participants
  • NASA
  • National Oceanic and Atmospheric Administration (NOAA)
  • Department of the Interior (DOI) U.S. Geological Survey (USGS)
  • Spacecraft bus: Lockheed Martin Missiles & Space
  • Enhanced Thematic Mapper (ETM): Hughes Santa Barbara Research Center

Launch
  • Date: October 5, 1993
  • Vehicle: Titan II
  • Launched by: NASA
  • Site: Western Test Range at Vandenberg Air Force Base, California

Spacecraft
  • Power provided by a single sun-tracking solar array and two 50 Ampere-Hour (AHr), Nickel Cadmium (NiCd) batteries
  • Attitude control provided through four reaction wheels (pitch, yaw, roll, and skew); three 2-channel gyros with celestial drift updating; a static Earth sensor; a 1750 processor; and torque rods and magnetometers for momentum uploading
  • Orbit control and backup momentum unloading provided through a blow-down monopropellant hydrazine system with a single tank containing 270 pounds of hydrazine, associated plumbing, and twelve 1-pound-thrust jets
  • Weight: approx. 4,800 lbs (2,200 kg)
  • Length: 4.3 m (14 ft)
  • Diameter: 2.8 m (9 ft)

Communications
  • Direct downlink with solid state recorders capable of storing 380 gigabits of data (100 scenes)
  • Data rate: 85 Mbps

Orbit (if obtained)
  • Worldwide Reference System-2 (WRS-2) path/row system
  • Sun-synchronous orbit at an altitude of 705 km (438 mi)
  • Inclined 98.2° (slightly retrograde)
  • Repeat cycle: 16 days
  • Equatorial crossing time: 10:00 a.m. +/- 15 minutes

Sensors
Enhanced Thematic Mapper (ETM)
  • Eight spectral bands, including a pan and thermal band:
    • Band 1 Visible (0.45 – 0.52 µm) 30 m
    • Band 2 Visible (0.52 – 0.60 µm) 30 m
    • Band 3 Visible (0.63 – 0.69 µm) 30 m
    • Band 4 Near-Infrared (0.76 – 0.90 µm) 30 m
    • Band 5 Near-Infrared (1.55 – 1.75 µm) 30 m
    • Band 6 Thermal (10.40 – 12.50 µm) 120 m
    • Band 7 Mid-Infrared (2.08 – 2.35 µm) 30 m
    • Band 8 Panchromatic (PAN) (0.52 - 0.90µm) 15 m
  • Ground Sampling Interval (pixel size): 30 m reflective, 120 m thermal

Other Characteristics
  • Scene size: 170 km x 185 km (106 mi x 115 mi)
sumber :
http://landsat.usgs.gov/about_landsat6.php

Sejarah Satelit Landsat 5

Landsat 5 History

March 1, 1984 – Present
August 1995 (Multispectral Scanner (MSS) powered off)
Landsat 5
Figure 1. Landsat 5

Participants
  • NASA
  • National Oceanic and Atmospheric Administration (NOAA)
  • Earth Observation Satellite Company (EOSAT)
  • Department of the Interior (DOI) U.S. Geological Survey (USGS)
  • Manufacturers: General Electric (GE) Astrospace and Hughes Santa Barbara Remote Sensing

Launch
  • Date: March 1, 1984
  • Vehicle: Delta 3920
  • Launched by: NASA
  • Site: Vandenberg Air Force Base, California

Spacecraft
  • 3-axis stabilized, zero momentum with control of 0.01 deg using reaction wheels
  • Aluminum with graphite struts
  • Hydrazine propulsion system
  • Single solar array with 1-axis articulation
  • Three Nickel Cadmium (NiCd) batteries provide 100 Ampere-Hour (AHr) total
  • Retractable boom (4 m long) with 2 powered joints supports the articulated High Gain Antenna, which downlinks data via Tracking and Data Relay Satellite System (TDRSS)
  • Communications system uses S,X,L, and Ku Bands
  • Weight: approximately 4,800 lbs (2,200 kg)

Communications
  • Direct downlink with TDRSS
  • Data rate: 85 Mbps
  • Quantisation: 8 bit (256 levels)

Orbit
  • Worldwide Reference System-2 (WRS-2) path/row system
  • Circular, sun-synchronous, near-polar orbit at an altitude of 705 km (438 mi)
  • Inclined at 98.2°
  • Repeat cycle: 16 days
  • Swath width: 185 km (115 mi)
  • Equatorial crossing time: 9:45 a.m. +/- 15 minutes

Sensors
Multispectral Scanner (MSS)
  • Four spectral bands (identical to Landsat 1 and 2):
    • Band 4 Visible green (0.5 to 0.6 µm)
    • Band 5 Visible red (0.6 to 0.7 µm)
    • Band 6 Near-Infrared (0.7 to 0.8 µm)
    • Band 7 Near-Infrared (0.8 to 1.1 µm)
  • Six detectors for each spectral band provided six scan lines on each active scan
  • Ground Sampling Interval (pixel size): 57 x 79 m
Thematic Mapper (TM)
  • Added the mid-range infrared to the data
  • Seven spectral bands, including a thermal band:
    • Band 1 Visible (0.45 – 0.52 µm) 30 m
    • Band 2 Visible (0.52 – 0.60 µm) 30 m
    • Band 3 Visible (0.63 – 0.69 µm) 30 m
    • Band 4 Near-Infrared (0.76 – 0.90 µm) 30 m
    • Band 5 Near-Infrared (1.55 – 1.75 µm) 30 m
    • Band 6 Thermal (10.40 – 12.50 µm) 120 m
    • Band 7 Mid-Infrared (2.08 – 2.35 µm) 30 m
  • Ground Sampling Interval (pixel size): 30 m reflective, 120 m thermal

Other Characteristics
  • Scene size: 170 km x 185 km (106 mi x 115 mi)
  • Design Life: Minimum of 3 years
sumber :
http://landsat.usgs.gov/about_landsat5.php

Sejarah Satelit Landsat 4

Landsat 4 History

July 16, 1982 – (placed in standby in January 1986) December 14, 1993
Decommissioned: June 15, 2001
Landsat 4
Figure 1. Landsat 4

Participants
  • NASA
  • National Oceanic and Atmospheric Administration (NOAA)
  • Earth Observation Satellite Company (EOSAT)
  • Department of the Interior (DOI) U.S. Geological Survey (USGS)

Launch
  • Date: July 16, 1982
  • Vehicle: Delta 3920
  • Launched by: NASA
  • Site: Vandenberg Air Force Base, California

Spacecraft
  • 3-axis stabilized, zero momentum with control of 0.01 deg using reaction wheels
  • Aluminum with graphite struts
  • Hydrazine propulsion system
  • Single solar array with 1-axis articulation
  • Three Nickel Cadmium (NiCd) batteries provide 100 Ampere-Hour (AHr ) total
  • Retractable boom (4 m long) with 2 powered joints supports the articulated High Gain Antenna, which downlinked data via the Tracking and Data Relay Satellite System (TDRSS)
  • Weight: approximately 4,300 lbs (1,942 kg)

Communications
  • Direct downlink with TDRSS
  • Data rate: 85 Mbps
  • Communications system uses S, X, L, and Ku Bands
  • Quantization: 8 bit (256 levels)

Orbit
  • Worldwide References System-2 (WRS-2) path/row system
  • Circular, sun-synchronous, near-polar orbit at an altitude of 705 km (438 mi)
  • Inclined at 98.2°
  • Circled the Earth every 99 minutes
  • Repeat cycle: 16 days
  • Equatorial crossing time: 9:45 a.m. +/- 15 minutes
  • Swath width: 185 km (115 mi)

Sensors
Multispectral Scanner (MSS)
  • Four spectral bands (identical to Landsat 1 and 2):
    • Band 4 Visible (0.5 to 0.6 µm)
    • Band 5 Visible (0.6 to 0.7 µm)
    • Band 6 Near-Infrared (0.7 to 0.8 µm)
    • Band 7 Near-Infrared (0.8 to 1.1 µm)
  • Data: 100 kHz digital
  • Six detectors for each reflective band provided six scan lines on each active scan
  • Ground Sampling Interval (pixel size): 57 x 79 m
Thematic Mapper (TM)
  • Added the mid-range infrared to the data
  • Seven spectral bands, including a thermal band:
    • Band 1 Visible (0.45 – 0.52 µm) 30 m
    • Band 2 Visible (0.52 – 0.60 µm) 30 m
    • Band 3 Visible (0.63 – 0.69 µm) 30 m
    • Band 4 Near-Infrared (0.76 – 0.90 µm) 30 m
    • Band 5 Near-Infrared (1.55 – 1.75 µm) 30 m
    • Band 6 Thermal (10.40 – 12.50 µm) 120 m
    • Band 7 Mid-Infrared (IR) (2.08 – 2.35 µm) 30 m
  • Ground Sampling Interval (pixel size): 30 m reflective, 120 m thermal

Other Characteristics
  • Scene size: 170 km x 185 km (106 mi x 115 mi)
  • Also known as Landsat-D
  • Design Life: Minimum of 3 years
Sumber :
http://landsat.usgs.gov/about_landsat4.php

Sejarah Satelit Landsat 3

Landsat 3 History

March 5, 1978 – March 31, 1983


Landsat 3
Figure 1. Landsat 3

Participants
  • NASA
  • Department of the Interior (DOI) U.S. Geological Survey (USGS)
  • Manufacturer: General Electric (GE) Astrospace

Launch
  • Date: March 5, 1978
  • Vehicle: Delta 2910
  • Launched by: NASA
  • Site: Vandenberg Air Force Base, California

Spacecraft
  • Weight: approximately 953 kg (2,100 lbs)
  • Overall height: 3 m (10 ft)
  • Diameter: 1.5 m (5 ft)
  • Solar array paddles extend out to a total of 4 m (13 ft)
  • 3-axis stabilized using 4 wheels to +/-0.7° attitude control
  • Twin solar array paddles (single-axis articulation)
  • S-Band and Very High Frequency (VHF) communications
  • Hydrazine propulsion system with 3 thrusters

Communications
  • Direct downlink from 2, 30 minute wide-band video tape recorders
  • Data rate: 15 Mbps
  • Quantization: 6 bit (64 levels)

Orbit
  • Worldwide Reference System-1 (WRS-1) path/row system
  • Sun-synchronous, near-polar orbit at an altitude of 917 km (570 mi)
  • Inclined at 99.1°
  • Circled the Earth every 103 minutes
  • Completed 14 orbits a day
  • Repeat cycle: 18 days
  • Swath width: 185 km (115 mi)
  • Equatorial crossing time: 9:30 a.m. +/- 15 minutes
  • Swath overlap (or sidelap) varied from 14 percent at the Equator to a maximum of approximately 85 percent at 81° north or south latitude

Sensors
Return Beam Vidicon (RBV)
  • The RBV system on Landsat 3 used two cameras, mounted side-by-side, with panchromatic spectral response and higher spatial resolution (40 m) to complement the multispectral coverage provided by the Multispectral Scanner (MSS). Each of the cameras produced a swath of about 90 km (for a total swath of 180 km).
  • 40 m resolution from 2, 80 m resolution cameras
  • Two cameras with a panchromatic spectral response
  • Data: 3.5 MHz video
Multispectral Scanner (MSS)
  • Five spectral bands, including a thermal band:
    • Band 4 Visible (0.5 to 0.6 µm)
    • Band 5 Visible (0.6 to 0.7 µm)
    • Band 6 Near-Infrared (0.7 to 0.8 µm)
    • Band 7 Near-Infrared (0.8 to 1.1 µm)
    • Band 8 Thermal (10.4 to 12.6 µm)
  • Data: 100 kHz digital
  • Six detectors for each reflective band provided six scan lines on each active scan
  • Ground Sampling Interval (pixel size): 57 x 79 m

Other Characteristics
  • Scene size: 170 km x 185 km (106 mi x 115 mi)
  • Originally designated Landsat 3; also known as Landsat C
  • Design Life: Minimum of 1 year
Sumber :
http://landsat.usgs.gov/about_landsat3.php

Sejarah Satelit Landsat 2

Landsat 2 History

January 22, 1975 - February 25, 1982 
Landsat 2
Figure 1. Landsat 2

Participants
  • NASA
  • Department of the Interior (DOI) U.S. Geological Survey (USGS)
  • Manufacturer: General Electric's (GE’s) Space Division in Valley Forge, Pennsylvania

Launch
  • Date: January 22, 1975
  • Vehicle: Delta 2910
  • Launched by: NASA
  • Site: Vandenberg Air Force Base, California

Spacecraft
  • Weight: approximately 953 kg (2,100 lbs)
  • Overall height: 3 m (10 ft)
  • Diameter: 1.5 m (5 ft)
  • Solar array paddles extend out to a total of 4 m (13 ft)
  • 3-axis stabilized using 4 wheels to +/-0.7° attitude control
  • Twin solar array paddles (single-axis articulation)
  • S-Band and Very High Frequency (VHF) communications
  • Hydrazine propulsion system with 3 thrusters

Communications
  • Direct downlink from 2, 30 minute wide-band video tape recorders
  • Data rate: 15 Mbps
  • Quantization: 6 bit (64 levels)

Orbit
  • Worldwide Reference System-1 (WRS-1) path/row system
  • Sun-synchronous, near-polar orbit at an altitude of 917 km (570 mi)
  • Inclined at 99.2°
  • Circled the Earth every 103 minutes
  • Completed 14 orbits a day
  • Repeat cycle: 18 days
  • Swath width: 185 km (115 mi)
  • Equatorial crossing time: 9:30 a.m. +/- 15 minutes
  • Swath overlap (or sidelap) varied from 14 percent at the Equator to a maximum of approximately 85 percent at 81° north or south latitude

Sensors
Return Beam Vidicon (RBV)
  • The RBV system on Landsat 2 was operated primarily for engineering evaluation purposes and only occasional RBV imagery was obtained, primarily for cartographic uses in remote areas.
  • 80 m resolution in the multispectral band
  • Three cameras that operate in the following spectral bands:
    • Visible blue-green (475-575 nm)
    • Visible orange-red (580-680 nm)
    • Visible red to Near-Infrared (690-830 nm)
  • Data: 3.5 MHz video

Multispectral Scanner (MSS)
  • Four spectral bands:
    • Band 4 Visible green (0.5 to 0.6 µm)
    • Band 5 Visible red (0.6 to 0.7 µm)
    • Band 6 Near-Infrared (0.7 to 0.8 µm)
    • Band 7 Near-Infrared (0.8 to 1.1 µm)
  • Six detectors for each spectral band provided six scan lines on each active scan
  • Ground Sampling Interval (pixel size): 57 x 79 m

Other Characteristics
  • Scene size: 170 km x 185 km (106 mi x 115 mi)
  • Originally designated ERTS-B (Earth Resources Technology Satellite-B), then named Landsat-2 prior to launch
  • Design Life: Minimum of 1 year
Sumber :
http://landsat.usgs.gov/about_landsat2.php

Sejarah Satelit Landsat 1

Landsat 1 History

July 23, 1972 - January 6, 1978




Landsat 1
Figure 1. Landsat 1

Participants
  • NASA
  • Department of the Interior (DOI) U.S. Geological Survey (USGS)
  • Manufacturer: General Electric's (GE’s) Space Division in Valley Forge, Pennsylvania

Launch
  • Date: July 23, 1972
  • Vehicle: Delta 900
  • Launched by: NASA
  • Site: Vandenberg Air Force Base, California

Spacecraft
  • Weight: approximately 953 kg (2,100 lbs)
  • Overall height: 3 m (10 ft)
  • Diameter: 1.5 m (5 ft)
  • Solar array paddles extend out to a total of 4 m (13 ft)
  • 3-axis stabilized using 4 wheels to +/-0.7° attitude control
  • Twin solar array paddles (single-axis articulation)
  • S-Band and Very High Frequency (VHF) communications
  • Hydrazine propulsion system with 3 thrusters

Communications
  • Direct downlink from 2, 30 minute wide-band video tape recorders
  • Data rate: 15 Mbps
  • Quantization: 6 bit (64 levels)

Orbit
  • Worldwide Reference System-1 (WRS-1) path/row system
  • Sun-synchronous, near-polar orbit at an altitude of 917 km (570 mi)
  • Inclined at 99.2°
  • Circled the Earth every 103.34 minutes
  • Completed 14 orbits a day
  • Repeat cycle: 18 days
  • Swath width: 185 km (115 mi)
  • Equatorial crossing time: 9:30 a.m. +/- 15 minutes
  • Swath overlap (or sidelap) varied from 14 percent at the Equator to a maximum of approximately 85 percent at 81° north or south latitude

Sensors
Return Beam Vidicon (RBV)
  • Operated from July 23, 1972 to August 5, 1972, recording only 1692 images
  • 80 m resolution in the multispectral band
  • Three cameras that operate in the following spectral bands:
    • Band 1 Visible blue-green (475-575 nm)
    • Band 2 Visible orange-red (580-680 nm)
    • Band 3 Visible red to Near-Infrared (690-830 nm)
  • Data: 3.5 MHz FM video
Multispectral Scanner (MSS)
  • Four spectral bands:
    • Band 4 Visible green (0.5 to 0.6 µm)
    • Band 5 Visible red (0.6 to 0.7 µm)
    • Band 6 Near-Infrared (0.7 to 0.8 µm)
    • Band 7 Near-Infrared (0.8 to 1.1 µm)
  • Six detectors for each spectral band provided six scan lines on each active scan
  • Ground Sampling Interval (pixel size): 57 x 79 m

Other Characteristics
  • Scene size: 170 km x 185 km (106 mi x 115 mi)
  • Originally designated ERTS-A (Earth Resources Technology Satellite); also known as ERTS-1 and Landsat-1
  • Program renamed Landsat in 1975
  • Design Life: Minimum of 1 year
Sumber :
http://landsat.usgs.gov/about_landsat1.php