Landsat 4 is the fourth satellite of the Landsat program. It was launched on July 16, 1982, with the primary goal of providing a global archive of satellite imagery. Although the Landsat Program is managed by NASA, data from Landsat 4 was collected and distributed by the U.S. Geological Survey. Landsat 4 science operations ended on December 14, 1993 when the satellite lost its ability to transmit science data, far beyond its designed life expectancy of five years. The satellite housekeeping telemetry and tracking continued to be maintained by NASA until it was decommissioned on June 15, 2001.
![]() Artist's rendering of Landsat 5, which is identical to Landsat 4. | |
Mission type | Earth imaging |
---|---|
Operator | NASA / NOAA |
COSPAR ID | 1982-072A ![]() |
SATCAT no. | 13367 |
Spacecraft properties | |
Bus | Multimission Modular Spacecraft |
Manufacturer | GE Astro Space |
Launch mass | 1,941 kilograms (4,279 lb) |
Dry mass | 1,407 kilograms (3,102 lb) |
Start of mission | |
Launch date | July 16, 1982 (1982-07-16) |
Rocket | Delta 3920 |
Launch site | Vandenberg AFB SLC-2W |
End of mission | |
Deactivated | June 15, 2001 (2001-06-16) |
Orbital parameters | |
Reference system | Geocentric |
Regime | Sun-synchronous |
Perigee altitude | 700 kilometers (430 mi) |
Apogee altitude | 704 kilometers (437 mi) |
Inclination | 98.2 degrees |
Period | 98.81 minutes |
Repeat interval | 16 days |
Epoch | August 17, 1982[1] |
Landsat 1, then known as ERTA-A, was launched July 23, 1972.[2] The satellite took over 100,000 images of the Earth over the course of its life.[3] Landsat 2 had a similar design, and was launched three years later.[4] Landsat 3, launched in 1978,[5] was the last satellite to have a similar design to Landsat 1, and was the last Landsat to be managed by NASA during the Landsat program.[2][6] Landsat 4 was the first Landsat to be operated by NOAA.[7]
The second generation of Landsat, Landsat 4 and 5, flew in lower orbits than the first three missions. Although they were in lower orbits, they had a higher field of view (FOV) so they had the same swath widths. The new Landsat spacecraft also featured improved instrumentation.[8]
The spacecraft was built by GE Astro Space, who would later become Lockheed Martin Missile and Space. It used the MultiMission Modular Spacecraft (MMS) bus developed by Fairchild Industries.[8][9]
The satellite was designed to be fixed by astronauts in space via the Space Shuttle, or taken back to Earth for repairs. It was expected that the shuttles would be able to reach Landsat's relatively far orbit by 1985.[7]
Landsat 4's attitude was controlled with hydrazine thrusters. The satellite was constructed with aluminum panels and graphite struts.[8] The spacecraft was three-axis stabilized with reaction wheels. It was powered by three nickel-cadmium batteries (NiCd), which were charged via a single solar array that had one axis of articulation. The solar array produced 1430 W of power.[8] The satellite weighed 4,300 pounds (2,000 kg). Landsat 4 was designed to last a minimum of three years.[10]
The satellite communicated to the ground with a direct downlink with the Tracking and Data Relay Satellite System (TDRSS) at 85 Mbit/s on the S-, X-, L-, and Ku-bands. The high gain antenna was extended with a retractable boom.[8] The data used 8 bit quantization.[10]
Landsat 4 carried an updated Multispectral Scanner (MSS), used on previous Landsat satellites, and a Thematic Mapper. It had a reflective resolution of 30 meters (98 ft) and a thermal resolution of 120 meters (390 ft).[10] Both were built by Hughes Aircraft.[9]
Landsat 4 was the first satellite in the Landsat program to incorporate the Thematic Mapper (TM) sensor. The Landsat TM sensor is able to gather seven bands of data as opposed to the four bands of data collected from the Multispectral Scanner. In addition to having three more bands of data to work with, scientists are able to view the TM data at a much higher resolution than with MSS. Bands 1–5 and 7 each have a spatial resolution of 30 meters (98 ft) while the MSS is only capable of a 57 meters (187 ft) by 79 meters (259 ft) resolution. Band 6 (which is a thermal infrared band) has a maximum spatial resolution of 120 meters (390 ft). The data rate for TM data was 84.9Mbit/s, via an X-band transmitter to modernized ground antennas.[8]
The satellite was launched from Vandenberg Air Force Base in California on July 16, 1982 on a Delta 3920.[10][11] Landsat 4 was placed into a north-south near polar orbit,[7] approximately 700 kilometers (430 mi) above Earth's surface, and circling the globe every 99 minutes.[10]
The first major malfunction occurred July 27, 1982. The high gain Ku antenna was commanded to deploy but failed. Attempts to free the antenna were successful on August 15.[8]
In February 1983, the satellite lost half of its solar power and the ability to send science data directly to Earth, prompting fears the satellite would fail sooner than expected.[12] This caused the early launch of Landsat 5, a satellite that was identical in specification to Landsat 4. After the issue was identified in Landsat 4, modifications were made to Landsat 5 to prevent the same issue from occurring.[12]
Landsat 4 was able to resume science operations when the Tracking and Data Relay Satellite System (TDRS) came online, then was placed in standby in January 1986.[10] Landsat 4 was brought back online to provide international coverage in 1987, when Landsat 5 lost its TDRS link, and thus the ability to image areas beyond line of sight to a ground station, and continued to do so until it, too, lost its TDRS link in 1993, ending science data return.[13] Landsat 4 continued to broadcast telemetry, tracking, and command data, which was transmitted on the still-functional S-band, until the satellite was decommissioned June 15, 2001.[10][14]
As early as 1982, a mission was in the planning stages to retrieve Landsat 4 for servicing back on earth. The 1982 edition of the STS Flight Assignment Manifest scheduled the second Space Shuttle mission from Vandenberg AFB for that task. The Space Shuttle orbiter Discovery was scheduled to launch on 15 June 1986 for a three day mission to capture Landsat 4 for return to earth (designated STS-2V). The following year, the mission was rescheduled to launch on 1 April 1986. Later on, the idea to retrieve Landsat 4 were first replaced by a servicing mission in early 1987, before any mention of it was removed from the flight manifest published in June 1985. The slot for the proposed mission was first assigned to a dedicated Space Shuttle flight for the Department of Defense before the idea of launching the Space Shuttle from Vandenberg AFB were scrapped altogether after the Challenger disaster.
← 1981 · Orbital launches in 1982 · 1983 → | |
---|---|
Kosmos 1331 | Kosmos 1332 | Kosmos 1333 | Satcom 4 | Kosmos 1334 | OPS 2849 | Kosmos 1335 | Kosmos 1336 |Ekran No.22L | Kosmos 1337 | Kosmos 1338 | Kosmos 1339 | Kosmos 1340 |Westar 4 | Molniya 1-53 | Kosmos 1341 | Taifun-2 | Intelsat V F-4 | Kosmos 1342 | OPS 8701 | Gorizont No.14L | Kosmos 1343 | STS-3 | Molniya 3-18 | Kosmos 1344 | Meteor 2-8 | Kosmos 1345 | Kosmos 1346 | Kosmos 1347 | Kosmos 1348 | Kosmos 1349 | INSAT-1A | Kosmos 1350 | Salyut 7 (Iskra 2) | Kosmos 1351 |Kosmos 1352 | Kosmos 1353 | Kosmos 1354 | Kosmos 1355 | Kosmos 1356 | Kosmos 1357 · Kosmos 1358 · Kosmos 1359 · Kosmos 1360 · Kosmos 1361 · Kosmos 1362 · Kosmos 1363 · Kosmos 1364 | OPS 5642 · OPS 6553 | Soyuz T-5 | Kosmos 1365 | Zenit-6 | Kosmos 1366 | Kosmos 1367 | Kosmos 1368 | Progress 13 | Kosmos 1369 | Kosmos 1370 | Molniya 1-54 | Kosmos 1371 | Kosmos 1372 | Kosmos 1373 | Kosmos 1374 | Kosmos 1375 | Kosmos 1376 | Kosmos 1377 | Westar 5 | Kosmos 1378 | Yantar-4K2 | Kosmos 1379 | Kosmos 1380 | Kosmos 1381 | Soyuz T-6 | Kosmos 1382 | STS-4 | Kosmos 1383 | Kosmos 1384 | Kosmos 1385 | Kosmos 1386 | Progress 14 | Kosmos 1387 | Landsat 4 | Kosmos 1388 · Kosmos 1389 · Kosmos 1390 · Kosmos 1391 · Kosmos 1392 · Kosmos 1393 · Kosmos 1394 · Kosmos 1395 | Molniya 1-55 | Ekran No.23L | Kosmos 1396 | Kosmos 1397 | Kosmos 1398 | Kosmos 1399 | Kosmos 1400 | Soyuz T-7 | Kosmos 401 | Anik D1 | Molniya 3-19 | Kosmos 1402 | Strela-2M | Kosmos 1403 | Kosmos 1404 | Kiku-4 | Kosmos 1405 | Kosmos 1406 | Marecs B · Sirio 2 | Fanhui Shi Weixing 0-5 | Kosmos 1407 | Kosmos 1408 | Ekran No.24L | Progress 15 (Astrozond) | Kosmos 1409 | Kosmos 1410 | Intelsat V F-5 | Kosmos 1411 | Kosmos 1412 | Kosmos 1413 · Kosmos 1414 · Kosmos 1415 | Kosmos 1416 | Kosmos 1417 | Gorizont No.16L | Kosmos 1418 | Satcom 5 | DSCS II F-16 · DSCS III A-1 | Progress 16 (Iskra 3) | Kosmos 1419 | Kosmos 1420 | STS-5 (SBS-3 · Anik C3) | OPS 9627 | Kosmos 1421 | Strela-1M (x8) | Gran' No.21L | Kosmos 1422 | Kosmos 1423 | Meteor 2-9 | Kosmos 1424 | OPS 9845 | Kosmos 1425 | Gran' No.22L | Kosmos 1426 | Kosmos 1427 | |
Payloads are separated by bullets ( · ), launches by pipes ( | ). Crewed flights are indicated in underline. Uncatalogued launch failures are listed in italics. Payloads deployed from other spacecraft are denoted in (brackets). |