INTELSAT II F-1

Overview

Destination: Geosynchronous Orbit
Mission: Communications

Geosynchronous Orbit Space Launch Complex 17B Cape Canaveral SFS, FL, USA

The Intelsat II series of satellites, first launched in 1966, marked the third generation of communications satellites developed by Hughes.

Thor Delta E1

Family:
Configuration: Delta E1

American orbital launch vehicle family with Thor first stage and a delta second stage.

Specifications
  • Stages
    4
  • Length
    28.0 m
  • Diameter
    2.44 m
  • Fairing Diameter
    2.44 m
  • Launch Mass
    68.0 T
  • Thrust
    1450.0 kN
Family
  • Name
    Thor Delta E1
  • Family
  • Variant
    Delta E1
  • Alias
  • Full Name
    Thor Delta E1
Payload Capacity
  • Launch Cost
  • Low Earth Orbit
    540.0 kg
  • Geostationary Transfer Orbit
    150.0 kg
  • Direct Geostationary
  • Sun-Synchronous Capacity

McDonnell Douglas

McDonnell Douglas

(MDC)

Successes: 0 Failures: 0 Pending: 0

Agency Type:

WIKI

Cape Canaveral SFS, FL, USA

Space Launch Complex 17B


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