Launch of an Athena I on the Kodiak Star mission.
|Function||Small expendable launch system|
|Country of origin||United States|
|Height||18.9 metres (62 ft)|
|Diameter||2.36 metres (7 ft 9 in)|
|Mass||66,300 kilograms (146,200 lb)|
|820 kilograms (1,810 lb)|
|360 kilograms (790 lb)|
|Launch sites||Kodiak LP-1
Spaceport Florida LC-46
Vandenberg SLC-6 & SLC-8
|First flight||Athena I: 15 August 1995
Athena Ic: 2012
|Last flight||Athena I: 30 September 2001|
|First Stage - Castor 120|
|Thrust||1,900 kilonewtons (430,000 lbf)|
|Specific impulse||280 sec|
|Burn time||83 seconds|
|Second Stage (Athena I) - Orbus 21D|
|Thrust||189.2 kilonewtons (42,500 lbf)|
|Specific impulse||293 sec|
|Burn time||150 seconds|
|Second Stage (Athena Ic) - Castor 30|
|Thrust||258.9 kilonewtons (58,200 lbf)|
|Specific impulse||294 sec|
|Burn time||143 seconds|
|Third Stage - OAM|
|Thrust||882 newtons (198 lbf)|
|Specific impulse||222 sec|
|Burn time||1,500 seconds|
The Athena I, known as the Lockheed Launch Vehicle (LLV) at the time of its first flight and Lockheed Martin Launch Vehicle (LMLV) at the time of its second flight, is an American small expendable launch system which was used for four launches between 1995 and 2001, and which is scheduled to return to service in 2012. It is a member of the Athena family of rockets, along with the larger Athena II. Launches from 2012 will use the Athena Ic configuration, which features a different second stage.
The Athena I is a three stage rocket, consisting of solid first and second stages, and a monopropellant liquid-fuelled third stage. The first stage is a Castor 120, which is also used on some versions of the Taurus rocket. An Orbus 21D motor was used as the second stage on launches up to 2001, however when it returns to service in 2012, the Castor 30, which is under development for the Taurus II, will be used instead. The third stage is an Orbital Adjustment Module, fuelled by hydrazine and propelled by four MR-107 engines, which is used for final insertion.
Prior to its retirement in 2001, Athena I launches were made from Space Launch Complex 6 at Vandenberg Air Force Base, Launch Complex 46 at Spaceport Florida, and Pad 1 of the Kodiak Launch Complex. The pads at Kodiak and Canaveral will be used for Athena Ic launches, with Launch Pad 0B of the Mid-Atlantic Regional Spaceport also offered. If a launch from Vandenberg is ordered, Space Launch Complex 8 will be used instead of SLC-6, which was rebuilt as a Delta IV launch complex following the Athena's initial retirement.
Four Athena I launches have been conducted, with one failure. Its maiden flight was conducted from SLC-6 at Vandenberg, and lifted off at 22:30 GMT on 15 August 1995. It was intended to place GemStar-1 into orbit, however the rocket was destroyed by the range safety officer after the failure of its thrust vectoring system resulted in a loss of control. The launch was the first from SLC-6, which had originally been built for the Titan III rocket for launches of the Manned Orbital Laboratory, and was later rebuilt for polar orbit Space Shuttle launches. Both MOL and polar Shuttle flights were cancelled before any launches were made from SLC-6. The next Athena I launch was on 23 August 1997, and successfully placed the Lewis satellite into orbit for NASA. This launch also took place from SLC-6 at Vandenberg. The third Athena I launch was from LC-46 at Spaceport Florida, and took place on 27 January 1999. The payload, ROCSAT-1, was the first satellite to be operated by the Republic of China. The fourth launch, which was conducted on 30 September 2001, was the first orbital launch to be made from Kodiak Island. Known as the Kodiak Star mission, it successfully placed the Starshine 3, Picosat 9, PCSat and Sapphire satellites into orbit.
- ALV X-1
- Comparison of small lift launch systems
- Comparison of solid-fuelled orbital launch systems
- Taurus II
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