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NEAR Shoemaker

File:NEAR_Shoemaker_spacecraft_model.png · Wikimedia Commons · See Wikimedia Commons

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NEAR Shoemaker

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Also known as Near Earth Asteroid Rendezvous - Shoemaker, Near Earth Asteroid Rendezvous, NEAR

1996 robotic space probe that landed on asteroid 433 Eros in 2001

Key facts

Mission type
Orbiter ( 433 Eros )
Operator
NASA · APL
Cospar id
1996-008A
Website
Official website
Mission duration
5 years, 21 days
Launch mass
805 kg
Dry mass
487 kilograms (1,074 lb)
Power
1,800 W
Launch date
February 17, 1996 ( 1996-02-17 ) 20:43:27 UTC
Rocket
Delta II 7925-8
Launch site
Cape Canaveral LC-17B
Last contact
February 28, 2001 ( 2001-02-28 ) ~00:00 UTC
Landing date
February 12, 2001 ( 2001-02-12 ) 20:01 UTC
Landing site
South of Himeros crater , 433 Eros
Closest approach
June 27, 1997 ( 1997-06-27 ) 12:56 UTC
Distance
1,212 kilometers (753 mi)
Orbital insertion
February 14, 2000 ( 2000-02-14 ) 15:33 UTC
Orbits
230 orbits

via Wikipedia infobox

Official website

Near Earth Asteroid Rendezvous Mission

Home of the Near Earth Asteroid Rendezvous (NEAR) Discovery Mission

near.jhuapl.edu

Link to the official site · 3,708 chars · not written by Vinony

~17 min read

Encyclopedic overview

Near Earth Asteroid Rendezvous – Shoemaker (NEAR Shoemaker), renamed after its 1996 launch in honor of planetary scientist Eugene Shoemaker, was a robotic space probe designed by the Johns Hopkins University Applied Physics Laboratory for NASA to study the near-Earth asteroid Eros from close orbit over a period of a year. It was the first spacecraft to orbit an asteroid and land on it successfully. In February 2000, the mission closed in on the asteroid and orbited it. On February 12, 2001, Shoemaker touched down on the asteroid and was terminated just over two weeks later.

The primary scientific objective of NEAR was to return data on the bulk properties, composition, mineralogy, morphology, internal mass distribution, and magnetic field of Eros. Secondary objectives include studies of regolith properties, interactions with the solar wind, possible current activity as indicated by dust or gas, and the asteroid spin state. This data was used to help understand the characteristics of asteroids in general, their relationship to meteoroids and comets, and the conditions in the early Solar System. To accomplish these goals, the spacecraft was equipped with an X-ray/gamma-ray spectrometer, a near-infrared imaging spectrograph, a multi-spectral camera fitted with a CCD imaging detector, a laser rangefinder, and a magnetometer. A radio science experiment was also performed using the NEAR tracking system to estimate the gravity field of the asteroid. The total mass of the instruments was 56 kg (123 lb), requiring 80 watts of power.

Excerpted from Wikipedia’s “NEAR Shoemaker” article, available under the CC BY-SA 4.0 licence.

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