Transtage 5

Overview

Destination: Low Earth Orbit
Mission: Test Flight

Low Earth Orbit Space Launch Complex 40 Cape Canaveral SFS, FL, USA

Test flights of the cryogenic Transtage stage.

Titan IIIC

Family:
Configuration: IIIC

The Titan IIIC was an expendable launch system used by the United States Air Force from 1965 until 1982. It was the first Titan booster to feature large solid rocket motors and was planned to be used as a launcher for the Dyna-Soar, though the spaceplane was cancelled before it could fly. The majority of the launcher's payloads were DoD satellites, for military communications and early warning, though one flight (ATS-6) was performed by NASA. The Titan IIIC was launched exclusively from Cape Canaveral while its sibling, the Titan IIID, was launched only from Vandenberg AFB.

Specifications
  • Minimum Stage
    2
  • Max Stage
    3
  • Length
    42.0 m
  • Diameter
    3.0 m
  • Fairing Diameter
    3.0 m
  • Launch Mass
    626.0 T
  • Thrust
    10586.0 kN
Family
  • Name
    Titan IIIC
  • Family
    ―
  • Variant
    IIIC
  • Alias
    ―
  • Full Name
    Titan IIIC
Payload Capacity
  • Launch Cost
    ―
  • Low Earth Orbit
    13100.0 kg
  • Geostationary Transfer Orbit
    3000.0 kg
  • Direct Geostationary
    ―
  • Sun-Synchronous Capacity
    ―

Lockheed Martin

Lockheed Martin

(LMT)

Founded: 1953 Successes: 77 Failures: 3 Pending: 0

Agency Type:

Lockheed Martin's Space Division started in the production of missiles and later ICBM's in the 1950s. Their TITAN missile system was used for 12 Gemini spacecraft and the Voyager probes. They have worked largely in collaboration with NASA on many of their probes, landers, and spacecraft, and hope to play a key role in NASA's return to the moon in 2024.

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