Thor family

Thor Delta B

RetiredUnited StatesMcDonnell DouglasSpec: Delta B

American orbital launch vehicle family with Thor first stage and a delta second stage.

Flights flown9
Success rate88.9%8/9
Payload to LEO370kg
Cost per kg to LEO$25,919$9.6M per launch
Maiden flight1962-12-13
Peak year19636 flights

Thor Delta B is built by McDonnell Douglas of the United States. It first flew on 13 December 1962 and last flew on 19 March 1964.

Flight record

9 records
88.9% success rate8 of 9 flown · 1 failed
1962peak 1963 · 6 flights1964
First flight1962-12-13
Latest flight1964-03-19
Failures1
Consecutive successes0
Fastest turnaround31d 11h

Payload

Per mission profile
Low Earth orbit370kg
Geostationary transfer orbit68kg
Launch cost$9.6M
Cost per kg to LEO$25,919

Vehicle

Delta B spec
Stages3
Length31m
Diameter2.44m
Launch mass51t
Liftoff thrust667kN
Maiden flight1962-12-13
ReusableNo

Pads used

2 pads

Orbits delivered

5 orbits
Elliptical Orbit2Geosynchronous Orbit2Low Earth Orbit2Sun-Synchronous Orbit2Medium Earth Orbit1

Launch history

9 launches
DateMissionPadOrbitOutcome
1964-03-19Thor Delta B | Beacon Explorer ASpace Launch Complex 17ALow Earth OrbitFailure
1964-01-21Thor Delta B | Relay 2Space Launch Complex 17BElliptical OrbitSuccess
1963-12-21Thor Delta B | Tiros 8Space Launch Complex 17BSun-Synchronous OrbitSuccess
1963-07-26Thor Delta B | Syncom 2Space Launch Complex 17AGeosynchronous OrbitSuccess
1963-06-19Thor Delta B | Tiros 7Space Launch Complex 17BSun-Synchronous OrbitSuccess
1963-05-07Thor Delta B | Telstar 2Space Launch Complex 17BMedium Earth OrbitSuccess
1963-04-03Thor Delta B | Explorer 17Space Launch Complex 17ALow Earth OrbitSuccess
1963-02-14Thor Delta B | Syncom 1Space Launch Complex 17BGeosynchronous OrbitSuccess
1962-12-13Thor Delta B | Relay 1Space Launch Complex 17AElliptical OrbitSuccess

Specifications from Launch Library 2 by The Space Devs, launch records from Space Index. Derived figures are computed here; see sources and method.

Further reading: Wikipedia