Rocket Details

In-depth specifications and launch history

Rocket placeholder

SM-65D Atlas

Atlas Family

About This Rocket

No detailed information available for this rocket.

Physical Specifications

Height25.15 m
Diameter3 m
Launch Mass119 kg
Stages1

Performance

LEO Capacity1,400 kg
GTO CapacityN/A kg
Thrust1,880 kN
Launch CostN/A

Manufacturer

Convair

CommercialUSAFounded 1943

Convair, previously Consolidated Vultee, was an American aircraft manufacturing company that later expanded into rockets and spacecraft. The company was formed in 1943 by the merger of Consolidated Aircraft and Vultee Aircraft. In 1953 it was purchased by General Dynamics, and operated as their Convair Division for most of its corporate history.

Total Launches

1

Success: 1Failed: 0

Success Rate

100.0%

Landing Success

0%

0/0 attempts

Consecutive Successes1

Technical Information

The SM-65D Atlas, or Atlas D, was the first operational version of the U.S. Atlas missile. Atlas D was first used as an intercontinental ballistic missile (ICBM) to deliver a nuclear weapon payload on a suborbital trajectory. It was later developed as a launch vehicle to carry a payload to low Earth orbit on its own, and later to geosynchronous orbit, to the Moon, Venus, or Mars with the Agena or Centaur upper stage.

ReusableNo

Launch Statistics

Maiden FlightApr 14, 1959
Total Launches9
Success: 6Failed: 3
Landing Success0/0

Additional Information

VariantD
Consecutive Successes0