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 7920-8
Part of Thor
American orbital launch vehicle. Three stage vehicle consisting of 9 x GEM-40 + 1 x EELT Thor/RS-27A + 1 x Delta K with 2.4 m (8 foot) diameter fairing)
Status: Active. First Launch: 1997-08-25. Last Launch: 1997-08-25. Number: 1 . Thrust: 4,000.00 kN (899,200 lbf). Gross mass: 220,000 kg (480,000 lb). Height: 39.00 m (127.00 ft). Diameter: 2.44 m (8.00 ft). Apogee: 400,000 km (240,000 mi).
More at: Delta 7920-8.
Family:
orbital launch vehicle.
Country:
USA.
Spacecraft:
ACE.
Launch Sites:
Cape Canaveral,
Cape Canaveral LC17A.
Stages:
Delta Thor XLT-C,
Delta K,
GEM 40.
Agency:
Douglas.
1997 August 25 - .
14:39 GMT - .
Launch Site:
Cape Canaveral.
Launch Complex:
Cape Canaveral LC17A.
LV Family:
Thor.
Launch Vehicle:
Delta 7920-8.
- ACE - .
Payload: ACE. Mass: 785 kg (1,730 lb). Nation: USA.
Agency: NASA Greenbelt.
Manufacturer: APL.
Class: Earth.
Type: Magnetosphere satellite. Spacecraft: ACE.
USAF Sat Cat: 24912 . COSPAR: 1997-045A. Apogee: 128,196 km (79,657 mi). Perigee: 176 km (109 mi). Period: 86,411.37 min. Earth-Sun L1 point.
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