Atlas-Agena

Atlas-Agena

An Atlas-Agena launching Lunar Orbiter 4
Function	Expendable launch system
Manufacturer	Convair General Dynamics
Country of origin	United States
Size
Height	118.0 feet (36.0 m)
Diameter	10.0 feet (3.0 m)
Width	16.0 feet (4.9 m)
Mass	341,000 pounds (155,000 kg)
Stages	2½
Capacity
Payload to LEO
Mass	2,200 pounds (1,000 kg)
Payload to GEO
Mass	1,540 pounds (700 kg)
Payload to TLI
Mass	850 pounds (390 kg)
Payload to escape
Mass	575 pounds (261 kg)
Launch history
Status	Retired
Launch sites	LC-12, 13 & 14, CCAFS SLC-3 & 4, Vandenberg
Total launches	109
Success(es)	93
Failure(s)	13
Partial failure(s)	3
First flight	26 February 1960
Last flight	27 June 1978
Boosters
No. boosters	1
Width	16.0 feet (4.9 m)
Powered by	2
Maximum thrust	233,000 pounds-force (1,040 kN)
Burn time	134 seconds
Propellant	RP-1/LOX
First stage
Diameter	10.0 feet (3.0 m)
Powered by	1
Maximum thrust	67,000 pounds-force (300 kN)
Burn time	5 minutes
Propellant	RP-1/LOX
Second stage – Agena D
Height	248 inches (6.3 m)
Diameter	5.0 feet (1.5 m)
Powered by	1 Bell Aerospace 8247
Maximum thrust	16,000 pounds-force (71 kN)
Burn time	265 seconds
Propellant	UDMH/IRFNA
[edit on Wikidata]

The Atlas-Agena was an American expendable launch system derived from the SM-65 Atlas missile. It was a member of the Atlas family of rockets, and was launched 109 times between 1960 and 1978.^[1] It was used to launch the first five Mariner uncrewed probes to the planets Venus and Mars, and the Ranger and Lunar Orbiter uncrewed probes to the Moon. The upper stage was also used as an uncrewed orbital target vehicle for the Gemini crewed spacecraft to practice rendezvous and docking. However, the launch vehicle family was originally developed for the Air Force and most of its launches were classified DoD payloads.

The Atlas-Agena was a two-and-a-half-stage rocket, with a stage-and-a-half Atlas missile as the first stage, and an RM-81 Agena second stage. Initially, Atlas D missiles, redesignated as the LV-3, were used as the first stage.^[2] These were later replaced by the standardized Atlas SLV-3, and its derivatives, the SLV-3A and B. The final Atlas-Agena launch used an Atlas E/F.

Launches were conducted from Launch Complexes 12, 13 and 14 at the Cape Canaveral Air Force Station, and Launch Complexes 1 and 2 at Point Arguello (now SLC-3 and 4 at Vandenberg Air Force Base).