Thor-Able

Last updated
  1. Krebs, Gunter. "Thor Able". Gunter's Space Page. Retrieved 2008-11-10.
  2. Wade, Mark. "Delta". Encyclopedia Astronautica. Archived from the original on 2013-08-17. Retrieved 2008-11-10.
  3. Wells, Helen T.; Whiteley, Susan H. & Karegeannes, Carrie E. (1976). Origins of NASA Names. NASA Science and Technical Information Office. p. 5. NASA SP-4402.
  4. Lethbridge, Cliff. "Thor-Able Fact Sheet". Cape Canaveral Rocket and Missile Programs. Spaceline. Archived from the original on 2007-06-13. Retrieved 2008-11-10.
LC-26B Thor-Able.jpg
Thor-Able on display at the Air Force Space & Missile Museum
Function Expendable launch system
Manufacturer Douglas/Aerojet
Country of originUnited States
Size
Height26.9 metres (88 ft) – 27.8 metres (91 ft)
Diameter2.44 metres (8 ft 0 in)
Mass51,608 kilograms (113,776 lb)
Stages2–3
Capacity
Payload to 640km LEO
Mass120 kilograms (260 lb)
Associated rockets
Family Thor
Derivative work Thor-Ablestar
Delta
Comparable Luna
Launch history
Launch sites LC-17A, Canaveral
Total launches9 suborbital
7 orbital
Success(es)7 suborbital
3 orbital
Failure(s)2 suborbital
4 orbital
First flight24 April 1958
Last flight1 April 1960
Type of passengers/cargo Pioneer
Transit
Tiros
First stage – Thor
Powered by1 LR79-7
Maximum thrust758.71 kilonewtons (170,560 lbf)
Specific impulse 282 seconds (2.77 km/s)
Burn time165 seconds
Propellant RP-1/LOX