Don Quijote (spacecraft)

Last updated
  1. 1 2 3 4 "Don Quixote concept". ESA. Archived from the original on 30 June 2015. Retrieved 17 June 2015.
  2. 1 2 3 4 5 6 "Sancho study: designing the minimum Earth escape spacecraft". ESA. 23 May 2012. Archived from the original on 15 May 2015. Retrieved 17 June 2015.
  3. 1 2 "Don Quijote mission". ESA . Retrieved 11 March 2023.
  4. "Don Quichotte". www.esa.int. Retrieved 2023-02-21.
  5. "NEO precursor studies". ESA. 26 February 2015. Archived from the original on 7 June 2015. Retrieved 17 June 2015.
  6. "N° 41–2005: ESA selects targets for asteroid-deflecting mission Don Quijote" (Press release). ESA. 26 September 2005. Retrieved 17 June 2015.
  7. "Asteroid Impact Deflection Assessment AIDA study". ESA. 26 February 2015. Archived from the original on 7 June 2015. Retrieved 17 June 2015.
  8. "Asteroid deflection mission seeks smashing ideas". ESA. 15 January 2013. Archived from the original on 21 June 2015. Retrieved 17 June 2015.
  9. "Asteroid Deflection Mission AIDA Set To Crash Two Spacecraft Into Space Rock In 2022". Huffington Post. 25 March 2013. Retrieved 17 June 2015.

Further reading

Don Quijote
Mission typeOrbiter, impactor, and lander
Operator European Space Agency
Website Don Quijote concept
Spacecraft properties
Bus Modified SMART-1 [1]
Launch massOrbiter: 491 kg (1,082 lb)
Lander: 1,694 kg (3,735 lb)
Dry massOrbiter: 395 kg (871 lb)
Lander: 532 kg (1,173 lb)
Payload massOrbiter: 20.6 kg (45 lb)
Lander: 9 kg (20 lb)
Start of mission
Launch dateStudied for a 2015 launch
Orbital parameters
Reference system Heliocentric
2003 SM84
or 99942 Apophis [2] orbiter
Spacecraft componentSancho
OrbitsMonths