Atlas

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Hero
Most launched

America''s first operational ICBM, transformed into the launch vehicle that carried John Glenn to orbit on Mercury-Atlas 6. The Atlas rocket family has been in continuous service for over 65 years, evolving through dozens of variants.

History

Karel Bossart''s Atlas was a radical design. Instead of using conventional thick-walled fuel tanks, Atlas used pressure-stabilized stainless steel tanks so thin that the rocket would collapse under its own weight if not pressurized -- like a metal balloon. This unusual approach saved enough weight to make the rocket viable as both an ICBM and a space launch vehicle.

Atlas entered service as America''s first operational intercontinental ballistic missile in 1959, capable of delivering a thermonuclear warhead to the Soviet Union. But its transformation into a space launcher would define its legacy far more than its military role. On February 20, 1962, an Atlas LV-3B carried John Glenn in the Mercury capsule Friendship 7 on three orbits of the Earth, making him the first American to orbit the planet.

The Atlas design has been continuously evolved ever since. Atlas-Centaur added the world''s first high-energy hydrogen upper stage. Atlas II and III served the commercial launch market. Atlas V, operated by United Launch Alliance, became one of the most reliable launch vehicles in history with over 100 consecutive successes. The Atlas lineage continued into the Vulcan Centaur, which inherited many Atlas V systems and procedures. No other rocket family can claim such longevity.

Timeline

1957First flight
1959Atlas entered service as America''s first operational intercontinental ballistic missile in 1959
19621962, an Atlas LV-3B carried John Glenn in the Mercury capsule Friendship 7 on three orbits of the Earth

Launch Heritage

Operational StatusRetired
Total Launches59/82 (72%)
Service Period1957-1968
DesignerKarel Bossart
Mission TypeICBM / Orbital launch
ReusabilityExpendable
Orbit TypeLEO
Target BodyEarth
Notable Missions
  • Mercury-Atlas 6
  • Mercury-Atlas 9
  • SCORE
  • Agena Target Vehicle

Technical Specifications

PropulsionLiquid (RP-1/LOX)
Height82.3 ft
Length82.3 ft
Diameter/Wingspan10 ft
Crew1
Gross Mass264,554 lbs

Propulsion

Engine ModelRocketdyne LR-105 (sustainer) + LR-89 (boosters) + LR-101 (verniers)
Engine Count5
Engine ManufacturerRocketdyne
Thrust1601 kN
Specific Impulse282 s
PropellantRP-1/LOX
Stages2

Performance

Payload to LEO820 kg

Dimensions

Height (m)25.1 m
Diameter (m)3.05 m
Length (m)25.1 m

Mass

Empty Mass (kg)5,395 kg
Gross Mass (kg)120,000 kg

Mission

Mission DurationFirst ICBM (1957), used for Mercury orbital flights, evolved into Atlas V/Atlas 500
Missions Flown300
Success Rate~250/300 (varied configs)
ReusableNo

Power & Systems

AvionicsBurroughs radio-inertial guidance system, ground-commanded
Communication BandC-band tracking radar

Source: USAF, NASA

Tags

Designed by Karel Bossart

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