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- Q49516 subject Q8372196.
- Q49516 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.".
- Q49516 countryOrigin Q30.
- Q49516 finalFlight "1981-10-06".
- Q49516 launchSite Q334465.
- Q49516 launchSite Q461492.
- Q49516 maidenFlight "1974-01-19".
- Q49516 rocketFunction Q15078724.
- Q49516 status "Retired".
- Q49516 successfulLaunches "43".
- Q49516 thumbnail Delta_2914_launching_IUE_spacecraft.jpg?width=300.
- Q49516 totalLaunches "44".
- Q49516 wikiPageWikiLink Q1034324.
- Q49516 wikiPageWikiLink Q1093806.
- Q49516 wikiPageWikiLink Q11241287.
- Q49516 wikiPageWikiLink Q1135571.
- Q49516 wikiPageWikiLink Q15078724.
- Q49516 wikiPageWikiLink Q15977211.
- Q49516 wikiPageWikiLink Q1751266.
- Q49516 wikiPageWikiLink Q2510100.
- Q49516 wikiPageWikiLink Q30.
- Q49516 wikiPageWikiLink Q334465.
- Q49516 wikiPageWikiLink Q4130.
- Q49516 wikiPageWikiLink Q461492.
- Q49516 wikiPageWikiLink Q46611.
- Q49516 wikiPageWikiLink Q48970.
- Q49516 wikiPageWikiLink Q49506.
- Q49516 wikiPageWikiLink Q49556.
- Q49516 wikiPageWikiLink Q51509.
- Q49516 wikiPageWikiLink Q5263733.
- Q49516 wikiPageWikiLink Q719315.
- Q49516 wikiPageWikiLink Q7337143.
- Q49516 wikiPageWikiLink Q7671215.
- Q49516 wikiPageWikiLink Q8372196.
- Q49516 first "1974-01-19".
- Q49516 function Q15078724.
- Q49516 last "1981-10-06".
- Q49516 launches "44".
- Q49516 name "Delta 2000 series".
- Q49516 sites Q1034324.
- Q49516 sites Q2510100.
- Q49516 sites Q334465.
- Q49516 sites Q461492.
- Q49516 status "Retired".
- Q49516 success "43".
- Q49516 type MeanOfTransportation.
- Q49516 type Rocket.
- Q49516 type DesignedArtifact.
- Q49516 type Thing.
- Q49516 type Q41291.
- Q49516 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.".
- Q49516 label "Delta 2000".
- Q49516 depiction Delta_2914_launching_IUE_spacecraft.jpg.
- Q49516 name "Delta 2000 series".