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 E
Part of Delta
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.
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