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

Status: Retired 1982. First Launch: 1965-11-06. Last Launch: 1967-04-20. Number: 6 . Thrust: 35.10 kN (7,890 lbf). Gross mass: 6,009 kg (13,247 lb). Unfuelled mass: 785 kg (1,730 lb). Specific impulse: 278 s. Burn time: 400 s. Height: 6.28 m (20.60 ft). Diameter: 1.40 m (4.50 ft). Span: 1.40 m (4.50 ft).

Cost $ : 2.320 million.


More at: Delta E.

Country: USA. Engines: AJ10-118E. Launch Vehicles: Thor Delta E, Thor Delta E1, Thor Delta G, Thor Delta J, Thor Delta N, Thor Delta M, Thor Delta L, Thor Delta N6, Thor Delta M6, N-1. Propellants: Nitric acid/UDMH.

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