An Atlas-Agena launches with the Agena for Gemini 6 in which it fails

The Agena Target Vehicle (ATV) was an unmanned spacecraft used by NASA during its Gemini program to develop and practice orbital space rendezvous and docking techniques and to perform large orbital changes, in preparation for the Apollo program lunar missions.[1]

Operations

An Atlas launch vehicle launches GATV-5006 into orbit for the Gemini 11 mission.

Each ATV consisted of an Agena-D derivative upper rocket stage built by Lockheed and a docking adapter built by McDonnell. The Agena was launched from Cape Canaveral Air Force Station Launch Complex 14 on top of an Atlas booster built by the Convair division of General Dynamics. The Agena first burn would occur shortly after shroud jettison and separation from the Atlas over the Atlantic Ocean. Over Ascension Island, a second burn would place the Agena into a low circular orbit.[1]

The McDonnell Gemini spacecraft would then be launched from Launch Complex 19, as soon as 90 minutes later. Both countdowns would proceed in parallel and required close synchronization. The Gemini would rendezvous and dock with the Agena as soon as Gemini's first orbit toward the end of the program.[1]

The Gemini astronauts would then fly the combined spacecraft in a stabilized mode and perform a number of experiments:

After the Gemini capsule separated for the last time, the Agena remained in orbit for a short time and was used to verify the command system.[clarification needed]

Augmented Target Docking Adapter

The ATDA in orbit as seen from Gemini 9A.

A backup vehicle for the ATV, known as the Augmented Target Docking Adapter (ATDA), was constructed by McDonnell from the docking target and the Gemini reentry attitude control thruster assembly for use if the primary ATV failed. The ATDA was designed to allow docking, but lacked the propulsion capability of the Agena rocket. The ATDA was used on Gemini 9A, after the Atlas-Agena launch vehicle failed. However, the Gemini 9 crew could not dock with the ATDA because the nose cone shroud failed to separate properly.The Gemini aacfshgbhj.[2]

Flight statistics

Target Gemini mission Launched Reentered NSSDC ID Mass Comments
GATV-5002 Gemini 6 October 25, 1965
15:00:04 UTC
October 25, 1965
15:06:20 UTC
GEM6T 7,190 pounds (3,260 kg) Atlas-Agena exploded during launch.
Gemini 6A achieved first rendezvous with Gemini 7 instead.
GATV-5003 Gemini 8 March 16, 1966
15:00:03 UTC
September 15, 1967 1966-019A 7,000 pounds (3,200 kg) Achieved first docking, but mission soon aborted due to stuck Gemini thruster.
ATV later used as secondary target on Gemini 10.
GATV-5004 Gemini 9 May 17, 1966
15:12:00 UTC
May 17, 1966
15:19:00 UTC
GEM9TA 7,170 pounds (3,250 kg) Failed to orbit.
ATDA No. 02186 Gemini 9A June 1, 1966
15:00:02 UTC
June 11, 1966 1966-046A 1,750 pounds (790 kg) No Agena rocket. Successful rendezvous, but no docking due to shroud separation failure.
GATV-5005 Gemini 10 July 18, 1966
20:39:46 UTC
December 29, 1966 1966-065A 7,000 pounds (3,200 kg) Boosted Gemini 10 to 412-nautical-mile (763 km) apogee.
GATV-5006 Gemini 11 September 12, 1966
13:05:01 UTC
December 30, 1966 1966-080A 7,000 pounds (3,200 kg) Boosted Gemini 11 to record 739.2-nautical-mile (1,369.0 km) apogee.
First demonstration of artificial gravity created in microgravity.
GATV-5001A Gemini 12 November 11, 1966
19:07:58 UTC
December 23, 1966 1966-103A 7,000 pounds (3,200 kg) No apogee boost due to defective Agena engine. Performed tether experiment.

See also

References

  1. ^ a b c d Lockheed Missiles & Space Company (1972-02-25). "Shuttle/Agena study. Volume 1: Executive summary". NASA.
  2. ^ "McDonnell ATDA". Encyclopedia Astronautica. Retrieved June 6, 2012.

Public Domain This article incorporates public domain material from websites or documents of the National Aeronautics and Space Administration.