Gemini-IX-A (9)

    Pad LC-19 ()
    Titan-II (9)
    EVA

    Crew:

    Thomas P. Stafford (2), Commander
    Eugene A. Cernan (1), Pilot

    Backup Crew:

    James A. Lovell Jr,
    Edwin E. Aldrin

    Capcoms:

    Edwin E. Aldrin, Jr. (Cape,Houston)
    Neil A. Armstrong (Houston)
    James A. Lovell, Jr. (Houston)
    Richard F. Gordon, Jr. (Houston)

    Milestones:

    Payload:

    Gemini-IX-A capsule

    Mission Objective:

    Primary objective was to perform rendezvous and docking and conduct EVA. Secondary objectives included: Rendezvous with ATDA (launched 6/1/66 from Complex 14) in 3rd revolution. Conduct systems evaluation and equiperiod rendezvous. Execute 7 experiments. Practice Docking, Rendezvous from above and to demonstrate controlled reentry. The original crew of Gemini-IX, Elliott M. See and Charles Bassett were killed in an airplane crash on February 28, 1966. The backup crew was named to the prime crew positions. Spacecraft weight: 3750kg. ATDA weight: 1088kg

    Launch:

    June 3, 1966 8:39:33.335 am EST. GT-9 was postponed when TLV 5303 with Gemini Agena target vehicle GATV-5004 malfunctioned on May 17. In its place, a substitute target was used for GT-9A; the Augmented Target Docking Adapter (ATDA) was launched by an Atlas on June 1, 1966 (TLV-5304) from Launch Complex 14; However GT-9A was not launched the same day as planned due to a guidance system computer problem. After a brief hold, the spacecraft was launched on the 3rd day.

    Orbit:

    Altitude: 311.5km (168nm)
    Inclination: 28.86 degrees
    Orbits: 45
    Duration: 3 Days, 0 hours, 20 min, 50 seconds
    Distance: km

    Landing:

    June 6, 1966. Landing was at 27deg 52min N and 75deg 0.4min West. Miss distance .704 miles (.38 nm). Recovery ship USS Wasp (crew onboard in 52 min).

    Mission Highlights:

    Primary objective of rendezvous and docking was only partially achieved because the shroud on the ATDA failed to jettison. Instead GT-9A performed a number of rendezvous maneuvers, including a simulation of lunar module rendezvous. EVA time 2hours 7 min. During EVA maneuvers, Cernan's visor became fogged, and he was unable to test the Air Force maneuvering unit.

    Secondary objective experiment S-10, Agena Micrometerorite Collection experiment was not attempted because EVA did not take place near Gemini Agena target vehicle (GATV).

    Click Here more information about Gemini-IX-A

    Click Here for Newer Missions

    Return to KSC Home Page Return to Gemini Page

    __________________________________________________________________

    Last Updated Friday August 25 13:03:58 EDT 2000 Jim Dumoulin (Redacted)