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 Thor ELT
Part of Thor DM-19
LOx/Kerosene propellant rocket stage. .

AKA: Extended Length Tank Thor. Status: Retired 1990. Thrust: 1,030.21 kN (231,600 lbf). Gross mass: 84,067 kg (185,336 lb). Unfuelled mass: 4,059 kg (8,948 lb). Specific impulse: 296 s. Specific impulse sea level: 262 s. Burn time: 222 s. Height: 22.40 m (73.40 ft). Diameter: 2.44 m (8.00 ft). Span: 2.44 m (8.00 ft).

Cost $ : 11.600 million.



Country: USA. Engines: RS-27. Launch Vehicles: Delta 1604, Delta 1914, Delta 1913, Delta 1900, Delta 2313, Delta 2310, Delta 2910, Delta 1410, Delta 1910, Delta 2913, N-1, N-2 (2), Delta 4000, Delta 4925-8. Propellants: Lox/Kerosene.

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