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
Delta D
Part of Delta Family
American orbital launch vehicle. Unaugmented Thor with Delta and solid propellant upper stages.

Status: Retired 1969. First Launch: 1964-08-19. Last Launch: 1965-04-06. Number: 2 . Thrust: 33.70 kN (7,575 lbf). Gross mass: 2,693 kg (5,937 lb). Unfuelled mass: 545 kg (1,201 lb). Specific impulse: 278 s. Burn time: 170 s. Height: 5.58 m (18.30 ft). Diameter: 0.84 m (2.75 ft). Span: 0.84 m (2.75 ft).

Cost $ : 1.160 million.


More at: Delta D.

Country: USA. Engines: AJ10-118D. Launch Vehicles: Thor Delta B, Thor Delta C, Thor Delta D, Thor Delta C1. Propellants: Nitric acid/UDMH.

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
© 1997-2017 Mark Wade - Contact
© / Conditions for Use