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Surveyor program

From Wikipedia, the free encyclopedia

Surveyor program
Surveyor 3 resting on the surface of the Moon, taken by Apollo 12 astronauts
Program overview
CountryUnited States
OrganizationNASA
PurposeDemonstrate soft landing on the Moon
StatusCompleted
Program history
CostUS$469 million
First flightMay 30–June 2, 1966
Last flightJanuary 7–10, 1968
Successes5
Failures2
Launch site(s)Cape Canaveral LC-36
Vehicle information
Launch vehicle(s)Atlas-Centaur

The Surveyor program was a NASA program that, from June 1966 through January 1968, sent seven robotic spacecraft to the surface of the Moon. Its primary goal was to demonstrate the feasibility of soft landings on the Moon. The Surveyor craft were the first American spacecraft to achieve soft landing on an extraterrestrial body. The missions called for the craft to travel directly to the Moon on an impact trajectory, a journey that lasted 63 to 65 hours, and ended with a deceleration of just over three minutes to a soft landing.[1]

The program was implemented by NASA's Jet Propulsion Laboratory (JPL) to prepare for the Apollo program, and started in 1960. JPL selected Hughes Aircraft in 1961 to develop the spacecraft system.[1] The total cost of the Surveyor program was officially $469 million.

Five of the Surveyor craft successfully soft-landed on the Moon, including the first one. The other two failed: Surveyor 2 crashed at high velocity after a failed mid-course correction, and Surveyor 4 lost contact (possibly exploding) 2.5 minutes before its scheduled touch-down.

All seven spacecraft are still on the Moon; none of the missions included returning them to Earth. Some parts of Surveyor 3 were returned to Earth by the crew of Apollo 12, which landed near it in 1969. The camera from this craft is on display at the National Air and Space Museum in Washington, DC.[2]

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Transcription

Goals

Astronaut Pete Conrad near Surveyor 3 during Apollo 12, 1969. Lunar Module in the background.

The program performed several other services beyond its primary goal of demonstrating soft landings. The ability of spacecraft to make midcourse corrections was demonstrated, and the landers carried instruments to help evaluate the suitability of their landing sites for crewed Apollo landings. Several Surveyor spacecraft had robotic shovels designed to test lunar soil mechanics. Before the Soviet Luna 9 mission (landing four months before Surveyor 1) and the Surveyor project, it was unknown how deep the dust on the Moon was. If the dust was too deep, then no astronaut could land. The Surveyor program proved that landings were possible. Some of the Surveyors also had alpha scattering instruments and magnets, which helped determine the chemical composition of the soil.

The simple and reliable mission architecture was a pragmatic approach to solving the most critical space engineering challenges of the time, namely the closed-loop terminal descent guidance and control system, throttleable engines, and the radar systems required for determining the lander's altitude and velocity. The Surveyor missions were the first time that NASA tested such systems in the challenging thermal and radiation environment near the Moon.

Launch and lunar landing

Launch of the Atlas-Centaur AC-10 rocket carrying the Surveyor 1 spacecraft, May 30, 1966

Each Surveyor mission consisted of a single unmanned spacecraft designed and built by Hughes Aircraft Company. The launch vehicle was the Atlas-Centaur, which injected the craft directly into trans-lunar flightpath. The craft did not orbit the Moon on reaching it, but directly decelerated from impact trajectory, from 2.6 km/s relative to the Moon before firing retrorockets to a soft landing about 3 minutes 10 seconds later.

Each craft was planned to slow to about 110 m/s (4% of speed before retrofire) by a main solid fuel retrorocket, which fired for 40 seconds starting at an altitude of 75.3 km above the Moon, and then was jettisoned along with the radar unit at 11 km from the surface. The remainder of the trip to the surface, lasting about 2.5 minutes, was handled by smaller doppler radar units and three vernier engines running on liquid fuels fed to them using pressurized helium. (The successful flight profile of Surveyor 5 was given a somewhat shortened vernier flight sequence as a result of a helium leak). The last 3.4 meters to the surface was accomplished in free fall from zero velocity at that height, after the vernier engines were turned off. This resulted in a landing speed of about 3 m/s. The free-fall to the surface was in an attempt to avoid surface contamination by rocket blast.

Surveyor 1 required a total of about 63 hours (2.6 days) to reach the Moon, and Surveyor 5 required 65 hours (2.7 days). The launch weights (at lunar injection) of the seven Surveyors ranged from 995.2 kilograms (2,194 lb) to 1,040 kilograms (2,290 lb), and their landing weights (minus fuel, jettisoned retrorocket, and radar unit) ranged from 294.3 kilograms (649 lb) to 306 kilograms (675 lb).

Missions

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Landing sites of American Surveyor and Apollo programs, together with Soviet Luna program.

Of the seven Surveyor missions, five were successful.

Surveyor No. Launched from Earth Arrived at Moon Disposition
1 May 30, 1966 June 2, 1966 landed on Oceanus Procellarum
2 September 20, 1966 September 23, 1966 crashed near Copernicus crater
3 April 17, 1967 April 20, 1967 landed on Oceanus Procellarum
4 July 14, 1967 July 17, 1967 crashed on Sinus Medii
5 September 8, 1967 September 11, 1967 landed on Mare Tranquillitatis
6 November 7, 1967 November 10, 1967 landed on Sinus Medii
7 January 7, 1968 January 10, 1968 landed near Tycho crater

Surveyor 6 was the first spacecraft planned to lift off from the Moon's surface. Surveyor 3 was the first spacecraft to unintentionally lift off from the Moon's surface, which it did twice, due to an anomaly with Surveyor's landing radar, which did not shut off the vernier engines but kept them firing throughout the first touchdown and after it. Apollo 12's Lunar Module Intrepid landed 600 feet from Surveyor 3, as planned. Surveyor 3's TV and telemetry systems were found to have been damaged by its unplanned landings and liftoffs.[2]

Space Race competition

An engineering model of Surveyor 3, S-10, used for thermal control tests. It was reconfigured to represent a flight model of Surveyor 3 or later, since it was the first to have a scoop and claw surface sampler. (National Air and Space Museum)

During the time of the Surveyor missions, the United States was actively involved in the Space Race with the Soviet Union. Thus, the Surveyor 1 landing in June 1966, only four months after the Soviet Luna 9 probe landed in February, was an indication the programs were at similar stages.[3]

See also

References

  1. ^ a b Kloman (1972). "NASA Unmanned Space Project Management - Surveyor and Lunar Orbiter" (PDF). NASA SP-4901.
  2. ^ a b https://nssdc.gsfc.nasa.gov/nmc/spacecraft/display.action?id=1967-035A – 24 January 2020
  3. ^ Reeves, Robert (1994). "Exploring the Moon". The superpower space race: An explosive rivalry through the solar system. Boston, MA, USA: Springer. pp. 101–130. doi:10.1007/978-1-4899-5986-7_4. ISBN 978-1-4899-5986-7.

External links

This page was last edited on 24 February 2024, at 02:04
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