Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
Thor Delta J
Part of Thor
Delta J no. 57
Delta J no. 57
Delta J no. 57 - COSPAR 1968-055
American orbital launch vehicle. Four stage vehicle consisting of 3 x Castor + 1 x Thor DSV-2C + 1 x Delta E + 1 x Star 37D

AKA: Delta J;Thrust Augmented Thor. Status: Retired 1968. First Launch: 1968-07-04. Last Launch: 1968-07-04. Number: 1 . Payload: 260 kg (570 lb). Thrust: 1,452.90 kN (326,625 lbf). Gross mass: 69,497 kg (153,214 lb). Height: 31.00 m (101.00 ft). Diameter: 2.44 m (8.00 ft). Apogee: 6,000 km (3,700 mi).

LEO Payload: 260 kg (570 lb). Payload: 263 kg (579 lb) to a GTO. Flyaway Unit Cost 1985$: 16.660 million.

Stage Data - Delta J



Family: orbital launch vehicle. Country: USA. Engines: AJ10-118E, AJ10-118J, MB-3-3. Spacecraft: RAE. Projects: Explorer. Launch Sites: Vandenberg, Vandenberg SLC2E. Stages: Delta Thor TA, Delta E, Castor 2, Star 37. Agency: Douglas.

1968 July 4 - . 17:26 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2E. LV Family: Thor. Launch Vehicle: Thor Delta J.

Back to top of page
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2019 Mark Wade - Contact
© / Conditions for Use