Delta II rocket: Difference between revisions
m Delta II moved to Delta II rocket |
PeterBrett (talk | contribs) mNo edit summary |
||
| Line 16: | Line 16: | ||
* [[Mars Odyssey]] (2001) | * [[Mars Odyssey]] (2001) | ||
* [[Mars Exploration Rovers]] - [[Spirit]] and [[Opportunity]] (2003) | * [[Mars Exploration Rovers]] - [[Spirit]] and [[Opportunity]] (2003) | ||
* [[Phoenix]] (2007) | |||
==External links== | ==External links== | ||
Revision as of 13:34, 18 November 2007
Overview

Delta II rocket systems are used in a variety of applications.
Delta II is the current operational configuration of the original Thor-Delta family of launch vehicles which were based on the Thor ICBM of the 1950's.
During the development of the Space Shuttle program, expendables such as Delta, Atlas and Titan were phased out. The Challenger accident (January 28, 1986), spurred renewed investment in expendable launch vehicles such as the Delta II.
Delta II rockets have successfully launched over 125 missions into Earth orbit including several Mars missions:
- Mars Global Surveyor (1996)
- Mars Pathfinder (1996)
- Mars Climate Orbiter (1998)
- Mars Polar Lander (1999)
- Mars Odyssey (2001)
- Mars Exploration Rovers - Spirit and Opportunity (2003)
- Phoenix (2007)