Viking 1 was the first of two spacecraft, along with Viking 2, each consisting of an orbiter and a lander, sent to Mars as part of NASA's Viking program.[2] The lander touched down on Mars on July 20, 1976, the first successful Mars lander in history. Viking 1 operated on Mars for 2307 days (over 61⁄4 years)[2] or 2245 Martian solar days, the longest Mars surface mission[2] until the record was broken by the Opportunity rover on May 19, 2010.[6]
![]() Viking orbiter/lander | |
Mission type | Orbiter and lander |
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Operator | NASA |
COSPAR ID | Orbiter: 1975-075A Lander: 1975-075C |
SATCAT no. | Orbiter: 8108 Lander: 9024 |
Website | Viking Project Information |
Mission duration | Orbiter: 1846 days (1797 sols) Lander: 2306 days (2245 sols) Launch to last contact: 2642 days |
Spacecraft properties | |
Manufacturer | Orbiter: NASA JPL Lander: Martin Marietta |
Launch mass | 3530 kg[lower-alpha 1] |
Dry mass | Orbiter: 883 kg (1,947 lb) Lander: 572 kg (1,261 lb) |
Power | Orbiter: 620 W Lander: 70 W |
Start of mission | |
Launch date | 21:22, August 20, 1975 (UTC) (1975-08-20T21:22Z)[2][3] |
Rocket | Titan IIIE/Centaur |
Launch site | LC-41, Cape Canaveral |
End of mission | |
Last contact | November 11, 1982 (1982-11-11)[4] |
Orbital parameters | |
Reference system | Areocentric |
Mars orbiter | |
Spacecraft component | Viking 1 Orbiter |
Orbital insertion | June 19, 1976[2][5] |
Orbital parameters | |
Periareion altitude | 320 km (200 mi) |
Apoareion altitude | 56,000 km (35,000 mi) |
Inclination | 39.3° |
Mars lander | |
Spacecraft component | Viking 1 Lander |
Landing date | July 20, 1976[2] 11:53:06 UTC (MSD 36455 18:40 AMT) |
Landing site | 22.27°N 312.05°E / 22.27; 312.05 (Viking 1 lander)[2] |
Flagship ← None |
Following launch using a Titan/Centaur launch vehicle on August 20, 1975, and an 11-month cruise to Mars,[7] the orbiter began returning global images of Mars about five days before orbit insertion. The Viking 1 Orbiter was inserted into Mars orbit on June 19, 1976,[8] and trimmed to a 1,513 x 33,000 km, 24.66 h site certification orbit on June 21. Landing on Mars was planned for July 4, 1976, the United States Bicentennial, but imaging of the primary landing site showed it was too rough for a safe landing.[9] The landing was delayed until a safer site was found,[9] and took place instead on July 20,[8] the seventh anniversary of the Apollo 11 Moon landing.[10] The lander separated from the orbiter at 08:51 UTC and landed at Chryse Planitia at 11:53:06 UTC.[11] It was the first attempt by the United States at landing on Mars.[12]
The instruments of the orbiter consisted of two vidicon cameras for imaging (VIS), an infrared spectrometer for water vapor mapping (MAWD) and infrared radiometers for thermal mapping (IRTM).[13] The orbiter primary mission ended at the beginning of solar conjunction on November 5, 1976. The extended mission commenced on December 14, 1976, after solar conjunction.[citation needed] Operations included close approaches to Phobos in February 1977.[14] The periapsis was reduced to 300 km on March 11, 1977.[15] Minor orbit adjustments were done occasionally over the course of the mission, primarily to change the walk rate — the rate at which the areocentric longitude changed with each orbit, and the periapsis was raised to 357 km on July 20, 1979. On August 7, 1980, Viking 1 Orbiter was running low on attitude control gas and its orbit was raised from 357 × 33943 km to 320 × 56,000 km to prevent impact with Mars and possible contamination until the year 2019. Operations were terminated on August 17, 1980, after 1,485 orbits. A 2009 analysis concluded that, while the possibility that Viking 1 had impacted Mars could not be ruled out, it was most likely still in orbit.[16] More than 57,000 images were sent back to Earth.
The lander and its aeroshell separated from the orbiter on July 20 at 08:51 UTC. At the time of separation, the lander was orbiting at about 5 kilometers per second (3.1 miles per second). The aeroshell's retrorockets fired to begin the lander de-orbit maneuver. After a few hours at about 300 kilometers (190 miles) altitude, the lander was reoriented for atmospheric entry. The aeroshell with its ablative heat shield slowed the craft as it plunged through the atmosphere. During this time, entry science experiments were performed by using a retarding potential analyzer, a mass spectrometer, as well as pressure, temperature, and density sensors.[13] At 6 km (3.7 mi) altitude, traveling at about 250 meters per second (820 feet per second), the 16 m diameter lander parachutes deployed. Seven seconds later the aeroshell was jettisoned, and 8 seconds after that the three lander legs were extended. In 45 seconds the parachute had slowed the lander to 60 meters per second (200 feet per second). At 1.5 km (0.93 mi) altitude, retrorockets on the lander itself were ignited and, 40 seconds later at about 2.4 m/s (7.9 ft/s), the lander arrived on Mars with a relatively light jolt. The legs had honeycomb aluminum shock absorbers to soften the landing.[13]
The landing rockets used an 18-nozzle design to spread the hydrogen and nitrogen exhaust over a large area. NASA calculated that this approach would mean that the surface would not be heated by more than one 1 °C (1.8 °F), and that it would move no more than 1 millimeter (0.04 inches) of surface material.[11] Since most of Viking's experiments focused on the surface material a more straightforward design would not have served.[citation needed]
The Viking 1 lander touched down in western Chryse Planitia ("Golden Plain") at 22.697°N 312.05°E / 22.697; 312.05[2][11] at a reference altitude of −2.69 kilometers (−1.67 mi) relative to a reference ellipsoid with an equatorial radius of 3,397 kilometers (2,111 mi) and a flatness of 0.0105 (22.480° N, 47.967° W planetographic) at 11:53:06 UTC (16:13 local Mars time).[17] Approximately 22 kilograms (49 lb) of propellants were left at landing.[11]
Transmission of the first surface image began 25 seconds after landing and took about four minutes (see below). During these minutes the lander activated itself. It erected a high-gain antenna pointed toward Earth for direct communication and deployed a meteorology boom mounted with sensors. In the next seven minutes the second picture of the 300° panoramic scene (displayed below) was taken.[18] On the day after the landing the first colour picture of the surface of Mars (displayed below) was taken. The seismometer failed to uncage, and a sampler arm locking pin was stuck and took five days to shake out. Otherwise, all experiments functioned normally.
The lander had two means of returning data to Earth: a relay link up to the orbiter and back, and by using a direct link to Earth. The orbiter could transmit to Earth (S-band) at 2,000 to 16,000 bit/s (depending on distance between Mars and Earth), and the lander could transmit to the orbiter at 16,000 bit/s.[19] The data capacity of the relay link was about 10 times higher than the direct link.[13]
The lander had two facsimile cameras; three analyses for metabolism, growth or photosynthesis; a gas chromatograph-mass spectrometer (GCMS); an x-ray fluorescence spectrometer; pressure, temperature and wind velocity sensors; a three-axis seismometer; a magnet on a sampler observed by the cameras; and various engineering sensors.[13]
The Viking 1 lander was named the Thomas Mutch Memorial Station in January 1981 in honour of Thomas A. Mutch, the leader of the Viking imaging team.[20] The lander operated for 2245 sols (about 2306 Earth days or 6 years) until November 11, 1982, (sol 2600), when a faulty command sent by ground control resulted in loss of contact. The command was intended to uplink new battery charging software to improve the lander's deteriorating battery capacity, but it inadvertently overwrote data used by the antenna pointing software. Attempts to contact the lander during the next four months, based on the presumed antenna position, were unsuccessful.[21] In 2006 the Viking 1 lander was imaged on the Martian surface by the Mars Reconnaissance Orbiter.[22]
Viking 1 carried a biology experiment whose purpose was to look for evidence of life. The Viking lander biological experiments weighed 15.5 kg (34 lbs) and consisted of three subsystems: the pyrolytic release experiment (PR), the labeled release experiment (LR), and the gas exchange experiment (GEX). In addition, independent of the biology experiments, Viking carried a gas chromatograph-mass spectrometer (GCMS) that could measure the composition and abundance of organic compounds in the Martian soil.[23] The results were surprising and interesting: the GCMS gave a negative result; the PR gave a negative result, the GEX gave a negative result, and the LR gave a positive result.[24] Viking scientist Patricia Straat stated in 2009, "Our (LR) experiment was a definite positive response for life, but a lot of people have claimed that it was a false positive for a variety of reasons."[25] Most scientists now believe that the data were due to inorganic chemical reactions of the soil; however, this view may be changing after the recent discovery of near-surface ice near the Viking landing zone.[26] Some scientists still believe the results were due to living reactions. No organic chemicals were found in the soil. However, dry areas of Antarctica do not have detectable organic compounds either, but they have organisms living in the rocks.[27] Mars has almost no ozone layer, unlike the Earth, so UV light sterilizes the surface and produces highly reactive chemicals such as peroxides that would oxidize any organic chemicals.[28] The Phoenix Lander discovered the chemical perchlorate in the Martian soil. Perchlorate is a strong oxidant so it may have destroyed any organic matter on the surface.[29] If it is widespread on Mars, carbon-based life would be difficult at the soil surface.
Gravitational time dilation is a phenomenon predicted by the theory of general relativity whereby time passes more slowly in regions of lower gravitational potential. Scientists used the lander to test this hypothesis, by sending radio signals to the lander on Mars, and instructing the lander to send back signals, in cases which sometimes included the signal passing close to the Sun. Scientists found that the observed Shapiro delays of the signals matched the predictions of general relativity.[30]
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Missions are ordered by launch date. Sign † indicates failure en route or before intended mission data returned. |
← 1974 · Orbital launches in 1975 · 1976 → | |
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Soyuz 17 | Kosmos 702 | Kosmos 703 | Landsat 2 | Kosmos 704 | Kosmos 705 | Kosmos 706 | Kosmos 707 | Molniya-2-12 | Starlette | SMS-2 | Kosmos 708 | Kosmos 709 | Intelsat IV F-6 | Taiyo | Kosmos 710 | Kosmos 711 · Kosmos 712 · Kosmos 713 · Kosmos 714 · Kosmos 715 · Kosmos 716 · Kosmos 717 · Kosmos 718 | OPS 2439 | Kosmos 719 | Kosmos 720 | Kosmos 721 · Nauka-5KSA No.4 | Kosmos 722 | Interkosmos 13 | Meteor-M No.31 | Kosmos 723 | Soyuz 7K-T No.39 | Kosmos 724 | Kosmos 725 | GEOS-3 | Kosmos 726 | RM-20 | Molniya-3 No.12 | Kosmos 727 | Kosmos 728 | OPS 4883 | Aryabhata | Kosmos 729 | Kosmos 730 | Molniya-1-29 | Explorer 53 | Anik A3 | Polluz · Castor | OPS 9435 · OPS 9436 | Kosmos 731 · Nauka-9KS No.2 | Intelsat IV F-1 | OPS 6226 | Soyuz 18 | Kosmos 732 · Kosmos 733 · Kosmos 734 · Kosmos 735 · Kosmos 736 · Kosmos 737 · Kosmos 738 · Kosmos 739 | Kosmos 740 | Kosmos 741 | DS-U3-IK No.5 | Kosmos 742 | Molniya-1 No.24 · SRET-2 | Venera 9 | OPS 6381 · P-226-1 | Nimbus 6 | Kosmos 743 | Venera 10 | OPS 4966 | Kosmos 744 | OSO-8 | Kosmos 745 | Kosmos 746 | Kosmos 747 | Kosmos 748 | Kosmos 749 | Molniya-2-13 | Meteor-2 No.1 | Apollo-Soyuz | DM-2 | Kosmos 750 | Kosmos 751 | Kosmos 752 | Ji Shu Shiyan Weixing 1 | Kosmos 753 | Cos-B | Kosmos 754 | Kosmos 755 | Viking 1 | Kosmos 756 | Symphonie 2 | Kosmos 757 | Molniya-1-31 | Kosmos 758 | Molniya-2-14 | Kiku 1 | Viking 2 | Kosmos 759 | Kosmos 760 | Kosmos 761 · Kosmos 762 · Kosmos 763 · Kosmos 764 · Kosmos 765 · Kosmos 766 · Kosmos 767 · Kosmos 768 | Meteor-M No.28 | Kosmos 769 | Kosmos 770 | Kosmos 771 | Intelsat IVA F-1 | Aura | Kosmos 772 | Kosmos 773 | Kosmos 774 | Explorer 54 | Kosmos 775 | OPS 5499 | Triad 2 | E-8-5M No.412 | GOES 1 | Kosmos 776 | Kosmos 777 | Kosmos 778 | Kosmos 779 | Molniya-3 No.13 | Soyuz 20 | Explorer 55 | Kosmos 780 | Kosmos 781 | Kosmos 782 | Fanhui Shi Weixing 2 | Kosmos 783 | Kosmos 784 | OPS 4428 · OPS 5547 | DAD-A · DAD-B | Interkosmos 14 | Kosmos 785 | Satcom 1 | OPS 3165 | Ji Shu Shiyan Weixing 2 | Kosmos 786 | Molniya-2-15 | Unnamed | Prognoz 4 | Gran' No.11L | Meteor No.38 | Molniya-3 No.15 | |
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). |