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- Delta_2000 abstract "The Delta 2000 series was an American expendable launch system which was used to conduct forty-four orbital launches between 1974 and 1981. It was a member of the Delta family of rockets. Several variants existed, which were differentiated by a four digit numerical code.The Delta 1000, 2000 and 3000 series used surplus NASA Apollo program rockets engines for its first and second stages.The first stage was an Extended Long Tank Thor, re-engined with the Rocketdyne RS-27 replacing the earlier MB-3-III engine. The RS-27 engine was a rebranded H-1 engine used in the Saturn 1B with minor changes. Three or nine Castor-2 solid rocket boosters were attached to increase thrust at lift-off. The Delta-P second stage used the TRW TR-201 engine. The TR-201 engine was a Lunar Module Descent Engine reconfigured for fixed thrust output. Launches which required a three-stage configuration in order to reach higher orbits used the Thiokol Star-37D or 37E upper stage as an apogee kick motor.Delta 2000 launches occurred from Space Launch Complex 2W at Vandenberg AFB and both pads of Launch Complex 17 at Cape Canaveral. Forty-three out of forty-four launches were successful. The single failure being the maiden flight (19 January 1974), which placed Skynet 2A into a useless orbit. A short circuit in an electronics package circuit board (on second stage) left the upper stages and satellite in an unstable low orbit (96 x 3,406 km x 37.6 deg) that rapidly decayed. An investigation revealed that a substandard coating had been used on the circuit board.".
- Delta_2000 countryOrigin United_States.
- Delta_2000 finalFlight "1981-10-06".
- Delta_2000 launchSite Cape_Canaveral_Air_Force_Station.
- Delta_2000 launchSite Vandenberg_Air_Force_Base.
- Delta_2000 maidenFlight "1974-01-19".
- Delta_2000 rocketFunction Expendable_launch_system.
- Delta_2000 status "Retired".
- Delta_2000 successfulLaunches "43".
- Delta_2000 thumbnail Delta_2914_launching_IUE_spacecraft.jpg?width=300.
- Delta_2000 totalLaunches "44".
- Delta_2000 wikiPageID "21550149".
- Delta_2000 wikiPageRevisionID "587262110".
- Delta_2000 caption "Launch of IUE on a Delta 2914 J-8".
- Delta_2000 failed "1".
- Delta_2000 first "1974-01-19".
- Delta_2000 function Expendable_launch_system.
- Delta_2000 hasPhotoCollection Delta_2000.
- Delta_2000 last "1981-10-06".
- Delta_2000 launches "44".
- Delta_2000 name "Delta 2000 series".
- Delta_2000 sites Cape_Canaveral_Air_Force_Station.
- Delta_2000 sites Cape_Canaveral_Air_Force_Station_Space_Launch_Complex_17.
- Delta_2000 sites Vandenberg_AFB_Space_Launch_Complex_2.
- Delta_2000 sites Vandenberg_Air_Force_Base.
- Delta_2000 status "Retired".
- Delta_2000 success "43".
- Delta_2000 subject Category:Delta_(rocket_family).
- Delta_2000 type MeanOfTransportation.
- Delta_2000 type Rocket.
- Delta_2000 type RocketEngine.
- Delta_2000 type DesignedArtifact.
- Delta_2000 comment "The Delta 2000 series was an American expendable launch system which was used to conduct forty-four orbital launches between 1974 and 1981. It was a member of the Delta family of rockets.".
- Delta_2000 label "Delta 2000".
- Delta_2000 label "Delta 2000".
- Delta_2000 label "Дельта-2000".
- Delta_2000 sameAs Delta_2000.
- Delta_2000 sameAs Delta_2000.
- Delta_2000 sameAs m.05h4h65.
- Delta_2000 sameAs Q49516.
- Delta_2000 sameAs Q49516.
- Delta_2000 wasDerivedFrom Delta_2000?oldid=587262110.
- Delta_2000 depiction Delta_2914_launching_IUE_spacecraft.jpg.
- Delta_2000 isPrimaryTopicOf Delta_2000.
- Delta_2000 name "Delta 2000 series".
