File:NEAR_Shoemaker_spacecraft_model.png · Wikimedia Commons · See Wikimedia Commons
NEAR Shoemaker
Sign in to saveAlso 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.