Rocket Details

In-depth specifications and launch history

Athena I

Athena I

Athena Family

About This Rocket

No detailed information available for this rocket.

Physical Specifications

Height18.9 m
Diameter2.36 m
Launch Mass66 kg
Stages3

Performance

LEO Capacity820 kg
GTO CapacityN/A kg
Thrust1,900 kN
Launch CostN/A

Manufacturer

Lockheed Martin

(LMT)

CommercialUSAFounded 1953

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.

Total Launches

80

Success: 77Failed: 3

Success Rate

96.3%

Landing Success

0%

0/0 attempts

Vehicle FamilyTitan | Agena
SpacecraftHubble | JUNO | InSight
Consecutive Successes38

Technical Information

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. It is a member of the Athena family of rockets, along with the larger Athena II.

ReusableNo

Launch Statistics

Maiden FlightAug 15, 1995
Total Launches4
Success: 3Failed: 1
Landing Success0/0

Additional Information

VariantI
Consecutive Successes3