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Double Asteroid Redirection Test

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Double Asteroid Redirection Test

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Also known as DART, NASA's Double Asteroid Redirection Test

first mission in NASA's Solar System Exploration program; impact of asteroid Dimorphos in 65803 Didymos system

Key facts

Names
DART
Mission type
Planetary defense test mission
Operator
NASA / APL
Website
dart .jhuapl .edu /Mission
Mission duration
10 months, 1 day
Spacecraft
DART impactor LICIACube CubeSat
Manufacturer
Applied Physics Laboratory of Johns Hopkins University
Launch mass
DART : 610 kg (1,340 lb) LICIACube : 14 kg (31 lb)
Dimensions
DART : 1.8 × 1.9 × 2.6 m (5.9 × 6.2 × 8.5 ft) ROSA : 8.5 × 2.4 m (27.9 × 7.9 ft) (each)
Power
6.6 kW
Launch date
24 November 2021, 06:21:02 ( 2021-11-24UTC06:21:02Z ) UTC
Rocket
Falcon 9 Block 5 B1063-3
Launch site
Vandenberg , SLC ‑ 4E
Contractor
SpaceX
Impact date
26 September 2022, 23:14 UTC
Spacecraft component
LICIACube (deployed from DART)
Closest approach
26 September 2022, ~23:17 UTC
Distance
56.7 km (35.2 mi)

via Wikipedia infobox

Wikidata facts

Official website
dart.jhuapl.edu
Image
DART spacecraft model 2.png
Show 4 more facts
Commons category
Double Asteroid Redirection Test
UTC date of spacecraft launch
2021-11-24
hashtag
DARTMission
price
324000000
Sources (7)

via Wikidata · CC0

~27 min read

Article

The Double Asteroid Redirection Test (DART) was a NASA space mission to test a method of planetary defense against near-Earth objects (NEOs). It was designed to assess how much a spacecraft impact can deflect an asteroid by hitting it head-on. The target asteroid, Dimorphos, is a 525 feet (160 m) wide moonlet of the asteroid Didymos; neither asteroid poses an impact threat to Earth, but their joint characteristics made them an ideal target.

Launched on 24 November 2021, the DART spacecraft collided with Dimorphos at 14,000 mph (23,000 km/h) on 26 September 2022 about 6.8 million miles (10.9 million kilometers) from Earth. The collision shortened Dimorphos's orbit around Didymos by 32 minutes, greatly in excess of the pre-defined success threshold of 73 seconds. Deflection resulted from the ejection of debris which caused a recoil that was substantially larger than the impact itself. The collision also very slightly increased the asteroid pair's orbital speed around the Sun—an effect directly relevant to the goal of planetary protection by changing an object's path through space.

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