Lockheed Martin
Atlas IIIA
IIIA
Retired
Overview
/01American orbital launch vehicle used between 2000 and 2005.
Manufacturer
Lockheed Martin
Variant
IIIA
Alias
N/A
Maiden Flight
May 24, 2000
Technical Specifications
/0252.8 m
Length
3.05 m
Diameter
0 t
Launch Mass
4149 kN
Liftoff Thrust
8640 kg
LEO Capacity
4055 kg
GTO Capacity
Launch Record
/032
Total Launches
2
Successful
0
Failed
100.0%
Success Rate
0
Attempted Landings
0
Successful Landings
0
Failed Landings
0
Consecutive Successes