Editing Mariner 1

{{Use mdy dates|date=December 2022}}
{{Short description|Failed NASA mission to Venus (1962)}}
{{good article}}
{{Infobox spaceflight
| name                  = Mariner 1
| image                 = Mariner 2 Engineering Model.jpg 
| image_caption         = Mariner 1 is identical in design with [[Mariner 2]]
| image_size            = 300px
| mission_type          = [[Venus]] flyby
| operator              = [[NASA]] / [[Jet Propulsion Laboratory|JPL]]
| mission_duration      = {{time interval|22 Jul 1962 09:21:23|22 Jul 1962 09:26:17|show=hms}}<br/><small>Failed to orbit</small>

| spacecraft_type       = [[Ranger program|Ranger]] Block I
| manufacturer          = [[Jet Propulsion Laboratory]]
| dry_mass              = 
| launch_mass           = {{convert|202.8|kg|lb}}
| power                 =

| launch_date           = {{start-date|July 22, 1962, 09:21:23|timezone=yes}} [[GMT]]
| launch_rocket         = [[Atlas-Agena|Atlas LV-3 Agena-B]]
| launch_site           = [[Cape Canaveral Air Force Station|Cape Canaveral]], [[Cape Canaveral Air Force Station Launch Complex 12|LC-12]]
| disposal_type         = Launch failure
| destroyed             = {{end-date|July 22, 1962, 09:26:17.5|timezone=yes}} [[GMT]]
| launch_contractor     =
| programme             = '''[[Mariner program]]'''
| previous_mission      = 
| next_mission          = [[Mariner 2]]
}}

'''Mariner 1''', built to conduct the first American [[planetary flyby]] of [[Venus]], was the first spacecraft of [[NASA]]'s interplanetary [[Mariner program]]. Developed by [[Jet Propulsion Laboratory]], and originally planned to be a purpose-built probe launched summer 1962, Mariner 1's design was changed when the [[Centaur (rocket stage)|Centaur]] proved unavailable at that early date. Mariner 1 (and its sibling spacecraft, [[Mariner 2]]), were then adapted from the lighter [[Ranger program|Ranger]] lunar spacecraft. Mariner 1 carried a suite of experiments to determine the temperature of Venus as well to measure [[magnetic fields]] and [[charged particle]]s near the planet and in [[interplanetary space]].

Mariner 1 was launched by an [[Atlas-Agena]] rocket from [[Cape Canaveral Launch Complex 12|Cape Canaveral's Pad 12]] on July 22, 1962. Shortly after [[Takeoff|liftoff]], errors in communication between the rocket and its ground-based [[guidance systems]] caused the rocket to veer off course, and it had to be destroyed by [[range safety]]. The errors were traced to a mistake in a specification of the hand-written guidance equations which were then subsequently codified in the computer program.

{{TOC limit|3}}

==Background==

[[File:Mariner 2 trajectory.jpg|thumb|Mariner II [[trajectory]] projected on the [[ecliptic plane]].]]

With the advent of the [[Cold War]], the two then-[[superpower]]s, the [[United States of America|United States]] and the [[Soviet Union]], both initiated ambitious space programs with the intent of demonstrating military, technological, and political dominance.<ref name=history/> The Soviets launched the [[Sputnik 1]], the first Earth orbiting satellite, on October 4, 1957. The Americans followed suit with [[Explorer 1]] on February 1, 1958, by which point the Soviets had already launched the first orbiting animal, [[Laika]] in [[Sputnik 2]]. Earth's orbit having been reached, focus turned to being the first to the Moon. The [[Pioneer program]] of satellites consisted of three unsuccessful lunar attempts in 1958. In early 1959, the Soviet [[Luna 1]] was the first probe to fly by the Moon, followed by [[Luna 2]], the first artificial object to impact the Moon.<ref name=encyclopedia/>

With the Moon achieved, the superpowers turned their eyes to the planets. As the closest planet to Earth, [[Venus]] presented an appealing interplanetary spaceflight target.<ref name=treasury/>{{rp|172}} Every 19 months, Venus and the Earth reach relative positions in their orbits around the Sun such that a minimum of fuel is required to travel from one planet to the other via a [[Hohmann Transfer Orbit]]. These opportunities mark the best time to launch exploratory spacecraft, requiring the least fuel to make the trip.<ref name=Hohnmann/>

The first such opportunity of the Space Race occurred in late 1957, before either superpower had the technology to take advantage of it. The second opportunity, around June 1959, lay just within the edge of technological feasibility, and [[United States Air Force|U.S. Air Force]] contractor [[TRW Inc.|Space Technology Laboratory]] (STL) intended to take advantage of it. A plan drafted January 1959 involved two spacecraft evolved from the first Pioneer probes, one to be launched via [[Thor-Able]] rocket, the other via the yet-untested [[Atlas-Able]].<ref name=DevPlan/> STL was unable to complete the probes before June,<ref name=Able34/> and the [[launch window]] was missed. The Thor-Able probe was repurposed as the deep space explorer ''[[Pioneer 5]]'', which was launched March 11, 1960, and designed to maintain communications with Earth up to a distance of {{cvt|20000000|mi}} as it traveled toward the orbit of Venus.<ref name=P5/> (The Atlas Able probe concept was repurposed as the unsuccessful [[Pioneer P-1|Pioneer Atlas]] Moon probes.)<ref name=ableseries/> No American missions were sent during the early 1961 opportunity. The Soviet Union launched [[Venera 1]] on February 12, 1961, and on May 19–20 became the first probe to fly by Venus; however, it had stopped [[transmitter|transmitting]] on February 26.<ref name=NSSDC-2/>

For the summer 1962 launch opportunity, NASA contracted [[Jet Propulsion Laboratory]] (JPL) in July 1960 <ref name=treasury/>{{rp|172}} to develop "Mariner A", a {{cvt|1250|lb}} spacecraft to be launched using the yet undeveloped [[Atlas-Centaur]]. By August 1961, it had become clear that the [[Centaur (rocket stage)|Centaur]] would not be ready in time. JPL proposed to NASA that the mission might be accomplished with a lighter spacecraft using the less powerful but operational [[Atlas-Agena]]. A hybrid of Mariner A and JPL's Block 1 [[Ranger program|Ranger]] lunar explorer, already under development, was suggested. NASA accepted the proposal, and JPL began an 11-month crash program to develop "Mariner R" (so named because it was a Ranger derivative). Mariner 1 was the first Mariner R to be launched.<ref name=report/>

==Spacecraft==

Three Mariner R spacecraft were built: two for launching and one to run tests, which was also to be used as a spare.<ref name=treasury/>{{rp|174}} Aside from its scientific capabilities, Mariner also had to transmit data back to Earth from a distance of more than {{cvt|26000000|mi}}, and to survive solar radiation twice as intense as that encountered in Earth orbit.<ref name=treasury/>{{rp|176}}

===Structure===

[[File:Diagram of Mariner 1.jpg|thumb|Diagram of Mariner 1]]
 
All three of the Mariner R spacecraft, including Mariner 1, weighed within {{cvt|3|lb}} of the design weight of {{cvt|447|lb}}, {{cvt|406|lb}} of which was devoted to non-experimental systems: maneuvering systems, fuel, and communications equipment for receiving commands and transmitting data. Once fully deployed in space, with its two solar panel "wings" extended, Mariner R was {{cvt|12|ft}} in height and {{cvt|16.5|ft}} across. The main body of the craft was hexagonal with six separate cases of electronic and electromechanical equipment:

*Two of the cases comprised the power system: [[switchgear]] that regulated and transmitted power from the 9800 [[solar cells]] to the {{cvt|33.3|lb}} rechargeable 1000 watt<ref name=NSSDC/> silver-zinc storage battery. 
*Two more included the [[radio receiver]], the three-[[watt]] transmitter, and control systems for Mariner's experiments. 
*The fifth case held electronics for [[digital signal|digitizing]] the [[analog signal|analog]] data received by the experiments for transmission. 
*The sixth case carried the three [[gyroscope]]s that determined Mariner's orientation in space. It also held the central computer and sequencer, the "brain" of the spacecraft that coordinated all of its activities pursuant to code in its [[memory bank]]s and on a schedule maintained by an electronic clock tuned into equipment on Earth.<ref name=treasury/>{{rp|175}}

At the rear of the spacecraft, a [[monopropellant]] (anhydrous [[hydrazine]]) 225 [[Newton (unit)|N]]<ref name=NSSDC/> rocket motor was mounted for course corrections. A nitrogen gas fueled stabilizing system of ten jet nozzles controlled by the onboard gyroscopes, Sun sensors, and Earth sensors, kept Mariner properly oriented to receive and transmit data to Earth.<ref name=treasury/>{{rp|175}}

The primary [[high gain antenna|high gain]] parabolic antenna was also mounted on the underside of Mariner and kept pointed toward the Earth. An [[omnidirectional antenna]] atop the spacecraft would broadcast at times that the spacecraft was rolling or tumbling out of its proper orientation, to maintain contact with Earth; as an unfocused antenna, its signal would be much weaker than the primary. Mariner also mounted small antennas on each of the wings to receive commands from ground stations.<ref name=treasury/>{{rp|175–176}}

Temperature control was both passive, involving insulated, and highly reflective components; and active, incorporating [[louver]]s to protect the case carrying the onboard computer. At the time the first Mariners were built, no [[test chamber]] existed to simulate the near-Venus solar environment, so the efficacy of these cooling techniques could not be tested until the live mission.<ref name=treasury/>{{rp|176}}

===Scientific package===
[[File:Mariner 1 in JPL's Spacecraft Assembly Facility.jpg|thumb|Mariner 1 in JPL's Spacecraft Assembly Facility]]

====Background====

At the time of the Mariner project's inception, few of Venus' characteristics were definitely known. Its opaque [[atmosphere of Venus|atmosphere]] precluded [[telescope|telescopic]] study of the ground. It was unknown whether there was water beneath the clouds, though a small amount of [[water vapor]] above them had been detected. The planet's [[rotation rate]] was uncertain, though JPL scientists had concluded through [[radar]] observation that Venus rotated very slowly compared to the Earth, advancing the long-standing<ref name=beyond1/> (but eventually disproven)<ref name=nasa1/> hypothesis that the planet was [[Tidal locking|tidally locked]] with respect to the Sun (as the Moon is with respect to the Earth).<ref name=avweek1961/> No oxygen had been detected in Venus' atmosphere, suggesting that life as existed on Earth was not present. It had been determined that Venus' atmosphere contained at least 500 times as much [[carbon dioxide]] as the Earth's. These comparatively high levels suggested that the planet might be subject to a [[runaway greenhouse effect]] with surface temperatures as high as {{cvt|600|K}}, but this had not yet been conclusively determined.<ref name=report/>{{rp|7–8}}

The Mariner spacecraft would be able to verify this hypothesis by measuring the temperature of Venus close-up;<ref name=avweek1960a/> at the same time, the spacecraft could determine if there was a significant disparity between night and daytime temperatures.<ref name=report/>{{rp|331}} An on-board [[magnetometer]] and suite of charged particle detectors could determine if Venus possessed an appreciable magnetic field and an analog to Earth's [[Van Allen Belts]].<ref name=avweek1960a/>

As the Mariner spacecraft would spend most of its journey to Venus in interplanetary space, the mission also offered an opportunity for long-term measurement of the [[solar wind]] of charged particles and to map the variations in the Sun's [[magnetosphere]]. The concentration of [[cosmic dust]] beyond the vicinity of Earth could be explored as well.<ref name=treasury/>{{rp|176}}

====Experiments====

Experiments for the measurement of Venus and interplanetary space included:

*A [[Microphone#Piezoelectric microphone|crystal microphone]] for measurement of the density of cosmic dust, mounted on the central frame.
*A [[proton]] detector for counting low-energy protons in the solar wind, also mounted on the central frame.
*Two [[Geiger–Müller tube|Geiger-Müller (GM) tubes]] and an [[ion chamber]], for measuring high-energy charged particles in interplanetary space and in the Venusian equivalent of Earth's Van Allen Belts (which were later shown not to exist). These were mounted on Mariner's long axis to avoid the magnetic fields of the control equipment as well as secondary radiation caused by [[cosmic rays]] hitting the metal structure of the spacecraft. 
*An Anton special-purpose GM tube, for measuring lower energy radiation, particularly near Venus, also mounted away from the central frame.
*A three-axis [[Spacecraft magnetometer#Fluxgate magnetometers|fluxgate magnetometer]]<ref name=NSSDC/> for measuring the Sun's and Venus' magnetic fields, also mounted away from the central frame.
*A microwave [[radiometer]], a {{cvt|20|in}} diameter, {{cvt|3|in}} deep, parabolic antenna designed to scan Venus up and down at two microwave wavelengths (19&nbsp;mm and 13.5mm), slowing down and reversing when it found a hot spot. The 19&nbsp;mm wavelength was for measuring the temperature of the planet's surface while the 13.5mm wavelength measured the temperature of Venus' cloudtops. The instrument was mounted just above the central frame.
*Two [[infrared]] optical sensors for parallel measurement of the temperature of Venus, one at 8 to 9 [[microns]], the other at 10-10.8 microns, also mounted above the central frame.{{r|treasury|report}}{{rp|9}}<ref name=avweek1960a/>

Not included on any of the Mariner R spacecraft was a camera for visual photos. With payload space at a premium, project scientists considered a camera an unneeded luxury, unable to return useful scientific results. [[Carl Sagan]], one of the Mariner R scientists, unsuccessfully fought for their inclusion, noting that not only might there be breaks in Venus' cloud layer, but "that cameras could also answer questions that we were way too dumb to even pose".<ref name=space.com1/>

===Flight plan and ground operations===

[[File:Woomera 1964 0(1).jpg|thumb|120px|The communications station at Woomera]]

The launch window for Mariner, constrained both by the orbital relationship of Earth and Venus and the limitations of the Atlas Agena, was determined to fall in the 51 day period from July 22 through September 10.<ref name=treasury/>{{rp|174}} The Mariner flight plan was such that the two operational spacecraft would be launched toward Venus in a 30-day period within this window, taking slightly differing paths such that they both arrived at the target planet within nine days of each other, between December 8 and 16.<ref name=avweek1962a/> Only Cape Canaveral Launch Complex 12 was available for the launching of Atlas-Agena rockets, and it took 24 days to ready an Atlas-Agena for launch. This meant that there was only a 27-day margin for error for a two-launch schedule.<ref name=treasury/>{{rp|174}}

Each Mariner would be launched into a [[parking orbit]], whereupon the restartable Agena would fire a second time, sending Mariner on its way to Venus (errors in [[trajectory]] would be corrected by a mid-course burn of Mariner's onboard engines).<ref name=report/>{{rp|66–67}} Real-time radar tracking of the Mariner spacecraft while it was in [[parking orbit]] and upon its departure the [[Atlantic Missile Range]] would provide real-time radar tracking with stations at [[Ascension Island|Ascension]] and [[Pretoria]], while [[Palomar Observatory]] provided optical tracking. Deep space support was provided by three tracking and communications stations at [[Goldstone Deep Space Communications Complex|Goldstone, California]], [[RAAF Woomera Range Complex|Woomera, Australia]], and [[Hartebeesthoek Radio Astronomy Observatory|Johannesburg, South Africa]], each separated on the globe by around 120° for continuous coverage.<ref name=report/>{{rp|231–233}}

== Launch failure ==

[[File:Atlas Agena with Mariner 1.jpg|thumb|Atlas Agena with Mariner 1]]

The launch of Mariner 1 was scheduled for the early morning of July 21, 1962. Several delays caused by trouble in the [[range safety]] command system delayed the beginning of the [[Countdown#Rocketry|countdown]] until 11:33&nbsp;p.m. [[Eastern Time Zone|EST]] the night before. At 2:20&nbsp;a.m., just 79 minutes before launch, a blown [[fuse (electrical)|fuse]] in the range safety circuits caused the launch to be canceled. Countdown was reset that night and proceeded, with several holds, planned and unplanned, from 11:08&nbsp;p.m., through the early morning of the next day.

At 9:21:23&nbsp;a.m. on July 22, 1962, Mariner 1's Atlas-Agena lifted off from LC-12. The launch went entirely according to plan up to booster separation. During sustainer phase, the guidance system began issuing improper steering instructions, causing the Atlas to fishtail left and right. Its flight trajectory began to point downward and to the left of where it was supposed to be, creating the danger that it could impact in the crowded Atlantic shipping lanes. At 9:26:16&nbsp;a.m., just six seconds before the Agena second stage was scheduled to separate from the Atlas, at which point destruction of the rocket was no longer possible, a [[range safety officer]] ordered the rocket to self-destruct, which it did--the Atlas Flight Termination System was also designed to destruct the Agena if activated but Agena had no Flight Termination System of its own and could not be destructed following Atlas SECO. Telemetry signals were received from the probe for another 1-1/2 minutes. Mariner program director Jack James believed the destruction of the rocket was unnecessary and it would not have landed anywhere but the middle of the ocean.<ref name=report/>{{rp|87}}

===Cause of the malfunction===
Because of the gradual rather than sharp deviation from its course, JPL engineers suspected the fault lay in the flight equations loaded into the [[SM-65 Atlas#Guidance|computer that guided Atlas-Agena]] from the ground during its ascent.<ref name=avweek1962a/> After five days of post-flight analysis, JPL engineers determined what had caused the malfunction on Mariner 1: an error in the guidance computer logic combined with a hardware failure.<ref name=ceruzzi/>

The Burroughs guidance computer used data transmitted to it from the rate beacon on the Atlas and used this information to issue steering commands. The guidance program was supposed to contain a hyphen which instructed the computer to ignore data coming from the Atlas's rate beacon if it failed in-flight to prevent incorrect commands from being sent but it had been accidentally left out of the program, which a technician at Cape Canaveral entered into the computer as it was without realizing the program he was sent had a mistake in it.{{r|ceruzzi|vice}} (The very same mistake that would afflict [[Phobos 1]] 26 years later).
 	
During its ascent, Mariner 1's booster briefly lost [[Missile guidance#Remote control guidance|guidance-lock]] with the ground. Because this was a fairly common occurrence, the Atlas-Agena was designed to continue on a preprogrammed course until guidance-lock with the ground resumed.<ref name=avweek1962b/> When lock was reestablished, however, the faulty guidance logic caused the program to erroneously report that the "velocity was fluctuating in an erratic and unpredictable manner", which the program tried to correct for, causing actual erratic behavior, which prompted the range safety officer to destroy the rocket.<ref name=ceruzzi/>

The incorrect logic had previously been used successfully for [[Ranger program|Ranger]] launches but the rate beacon had not malfunctioned on those so the problem didn't show up there. The Mod III-G guidance system used on Atlas-Agena vehicle was a persistent source of trouble and malfunctioned on many launches since Atlas-Agena began flying in 1960. It was an adaption of the Mod III guidance system used on Atlas B, C, and D missiles which had the original vacuum tube electronics converted to transistors, but the modification had been done hastily and was unreliable. After repeated Atlas-Agena guidance failures, the Mod III-G was redesigned during 1963 to properly accommodate transistor electronics.<ref name=ceruzzi/>

The catastrophic effects of a small error "summed up the whole problem of software reliability" and contributed to the development of the discipline of [[software engineering]].<ref name=ceruzzi/>

Subsequent popular accounts of the accident often referred to the erroneous character as a "hyphen" (describing the missing component of the symbol) rather than an "R-bar"; this incorrect mischaracterization was fueled by [[Arthur C. Clarke]]'s description of the malfunction as "the most expensive hyphen in history".<ref name=vice/>

==Legacy==

The loss of America's first interplanetary spacecraft constituted an $18.5 million (${{Formatprice|{{Inflation|US|18500000|1962}}}} in today's dollars) setback for NASA.<ref name=tao/> The incident underscored the importance of a thorough pre-launch debugging of software as well as a need to engineer programs such that minor errors could not cause catastrophic failures. The procedures implemented as a result served NASA well, ultimately salvaging the [[Project Apollo]] Moon landings; though there were program errors in the [[Lunar Excursion Module]] software during descent, they did not cause mission failure.<ref name=timeand/>

With the logic error quickly discovered,<ref name=floss/> no undue delay was necessary. The identical [[Mariner 2]] was already on hand, and a second launch from the same pad was manageable before the end of August.<ref name=Tribune/> On August 27, 1962, Mariner 1's sister spacecraft was successfully launched, becoming on December 14, 1962, the first spacecraft to return data from the vicinity of Venus.<ref name=treasury/>{{rp|171,177}}

==See also==
{{Portal|Spaceflight}}
* [[List of missions to Venus]]
* [[List of software bugs#Space|List of software bugs]]

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| website= Space.com
| archive-date= 25 July 2022
| archive-url= https://web.archive.org/web/20220725005155/https://www.space.com/18746-mariner-2.html
| url-status= live }}
</ref>

<ref name="tao">{{cite book
| url= https://books.google.com/books?id=NDbQe52pX3kC&pg=PA130
| title= The Tao of Computing
| author1= Henry Walker
| date= 2005
| publisher= Jones and Bartlett Publishers, Inc.
| location=Sudbury, MA
| isbn=978-0-763-72552-5
| page= 130
| oclc= 864860042 }}
</ref>

<ref name="timeand">{{cite web
| url= https://timeandnavigation.si.edu/navigating-space/challenges/mariner-1-destroyed
| title= Mariner 1 Destroyed
| website= timeandnavigation.si.edu
| publisher= [[Smithsonian]]
| access-date= 5 September 2021 }}
</ref>

<ref name="treasury">{{cite book
| title= The New Treasury of Science
| chapter= The Voyage of Mariner II
| editor1= Harlow Shapley
| editor2= Samuel Rapport
| editor3= Helen Wright
| author1= J. N. James
| location= New York
| publisher= Harper & Row
| date= 1965
| pages= 171–187
| isbn= 978-0-060-13835-6 }}
</ref>

<ref name="Tribune">{{cite news
| url= https://www.newspapers.com/clip/84860023/venus-rocket-flight-ends-in-fiery-failur/
| title=Venus Rocket Flight Ends in Fiery Failure
| date= 23 July 1962
| newspaper= [[Chicago Tribune]]
| page= 22
| via=Newspapers.com
| agency= UPI }}
</ref>

<ref name="vice">{{cite web
| url= https://www.vice.com/en/article/sometimes-a-typo-means-you-need-to-blow-up-your-spacecraft/
| title= Sometimes a Typo Means You Need to Blow Up Your Own Spacecraft
| author1= Alex Pasternack
| website= Vice.com
| date= 26 July 2014
| access-date= 1 July 2021 }}
</ref>

}}

== External links ==
* [https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=MARIN1 NASA's article about the Mariner I]
* [https://web.archive.org/web/20141205024557/http://solarsystem.nasa.gov/missions/profile.cfm?MCode=Mariner_01 Mariner 1 Mission Profile] by [http://solarsystem.nasa.gov NASA's Solar System Exploration]
* [[RISKS Digest]] [http://catless.ncl.ac.uk/Risks/8.75.html#subj1 detail about the Mariner I failure]

{{Mariner program | before=None| after=[[Mariner 2]]}}
{{Orbital launches in 1962}}

[[Category:Missions to Venus]]
[[Category:Mariner program]]
[[Category:Spacecraft launched in 1962]]
[[Category:Satellite launch failures]]
[[Category:Spacecraft launched by Atlas-Agena rockets]]
[[Category:Software bugs]]

[[de:Mariner#Mariner 1 und 2]]