Atlas

An Atlas A missile stands ready
for launch down the Atlantic Missile Range in 1957-1958. The Atlas A was
the first RD configuration that ultimately led to the operational Atlas D,
E, and F missiles. It consisted of minimum propellant, propulsion, and
guidance systems. Its maximum range was only 600 nautical miles, and its
maximum altitude was 57.5 nautical miles. A total of eight Atlas As were
launched--all on the Atlantic Missile Range--during the period June 1957
to June 1958.
The
Atlas rocket, famous for carrying the Mercury astronauts into orbit and
respected for its later role as the workhorse of the commercial satellite
launch industry, began as a modest proposal for winged and rocket-powered
missiles just weeks after the end of World War II. The vehicle that
evolved became the United States' first intercontinental ballistic missile
(ICBM) and a dependable space launch system that is still going strong at
the start of the new millennium.
In
October 1945, the U.S. Army Air Forces (USAAF) (predecessor of the modern
U.S. Air Force) invited the aerospace industry to submit proposals for the
development of four different varieties of missiles to deliver a warhead
against targets as far as 5,000 miles (8,047 kilometres) away. Within a
few months, the field had been narrowed to two different concepts: a
jet-powered, subsonic winged vehicle, and a rocket-powered, supersonic
ballistic missile.
On April
19, 1946, a contract was awarded to the Consolidated Vultee Aircraft
Corporation (Convair) to study each concept. Cutbacks in the national
defence budget triggered a corresponding reduction in missile development
funding and, in June 1947, the USAAF cancelled Convair's research contract;
however, the company was permitted to spend its remaining funds to finish
constructing three missile test vehicles and continue investigating
missile guidance and nosecone concepts.
Spurred
by the outbreak of the Korean conflict, the U.S. Air Force again received
funding to advance the development of a missile system and, by September
1951, determined that a ballistic rocket design was preferable to a winged
vehicle concept. A new contract was awarded to Convair (which became the
Convair division of General Dynamics Corporation in 1953) to investigate
technologies and provide solutions for the systematic, then accelerated,
development of a ballistic missile system, dubbed by Convair as "Project
Atlas."
In
January 1955, the Air Force ordered the Atlas (still referred to by its
code name, Weapon System WS107A-I) into production. President Dwight
Eisenhower and his National Security Council were briefed on the specifics
of the Atlas project on June 28, 1955, and within weeks, the president
designated the development of the Atlas to be of the “highest national
priority.”
Convair
was awarded a contract in September 1955 to begin producing the Atlas, and
by June 1956, the company began testing the missile's propulsion system
and electrical components. Convair would produce the Atlas' airframe and
integrate all of the missile's components, North American Aviation
manufacture the rocket engines, and General Electric fabricate the
missile's nosecone and jointly develop the Atlas' guidance system with the
A.C. Spark Plug Company.
The key
to the Atlas design is an extremely lightweight structure, conceived
largely by an inventive Convair engineer, Karl J. Bossart. The missile's
frame consisted of a very thin-gauge stainless-steel skin that maintains
its shape and structural integrity only from the high pressure inside its
propellant tanks. If the tank pressurization failed, the skin would
crumble and the launch vehicle would collapse under its own weight. Many
engineers, including famed rocket designer Wernher von Braun, worried that
the Atlas' design could not survive the intense aerodynamic stresses
placed upon it the early phases of launch, so much so that von Braun's
design team derisively referred to the Atlas as a “blimp” or their
“inflated competition.”
The
basic Atlas vehicle, remarkably unchanged almost 50 years after its
inception, is a 1˝ stage liquid-propellant launch vehicle consisting of a
booster section and a sustainer section, a unique configuration that
enables the missile to launch itself into orbit. The single rocket engine
in the sustainer section and the twin rocket engines in the booster
section all ignite at liftoff to propel the vehicle for the first two
minutes of flight; after which the two booster section engines are
jettisoned as the single sustainer engine continues to burn and carries
the vehicle into space.
Early
test models of the Atlas (designated the Atlas Series A) were 75 feet (23
meters) in length and 10 feet (3 meters) in diameter, powered by only the
two booster section rocket engines, with a maximum range of just 600
nautical miles (1,111 kilometres). The missiles were outfitted with a
dummy warhead, but lacking the sustainer engine, they were only capable of
reaching an altitude of 57.5 nautical miles (106.5 kilometres).
The
first Atlas test flight, a “Series A” missile, lifted off from Cape
Canaveral's Launch Complex 14 on June 11, 1957. The flight lasted only 24
seconds. The twin rocket engines lost thrust about 10,000 feet (3,048
meters) above the launch pad, the missile made a few pirouettes, and then
the Range Safety Officer transmitted a destruct signal commanding the
Atlas to blow itself up.
This
first launch failure, though disappointing, also contained a silver
lining. As the missile was tumbling out of control, the Atlas' frame and
thin skin remained intact, even though subjected to several seconds of
very high aerodynamic stress (or structural “loads”) far in excess of its
design limitations. This validated its structural integrity and ended the
controversy over its unconventional design. In all, a total of eight Atlas
Series A missiles were launched from June 1957 though June 1958.
Subsequent test versions (the “B” and “C” models) were launched in 1958
and 1959, and the Atlas D, the U.S.' first ICBM, became a functional
weapon system in January 1959 when the first Atlas ICBM squadron at
Vandenberg Air Force Base, California was activated, even before the first
successful launch of the Atlas D. The Air Force formally accepted the
Atlas on September 1, 1959, and the missile was declared "operational"
about a week later when an Atlas D ICBM was successfully launched from
Vandenberg.
During
the same timeframe, the Atlas missile was also proving its worth as a
space launch vehicle. Project Score-an Atlas B missile that launched
itself into low-Earth-orbit on December 18, 1958-carried an
instrumentation package developed by the U.S. Army Signal Corps that
became the world's first communications satellite by broadcasting a
recorded Christmas message from President Eisenhower back to Earth.
Atlas
model D, E, and F ICBMs, outfitted with nuclear warheads, were deployed at
Air Force bases throughout the United States, stored vertically in
underground silos and raised by elevators to an above-ground position for
launch. In addition to the original squadron at Vandenberg AFB, Atlas
ICBMs were deployed at eight locations in central and western United
States and at Plattsburg AFB, New York. (Plattsburg AFB still is the only
ICBM installation ever located east of the Mississippi River).
Atlas
ICBMs remained on strategic alert from 1959 until 1966, when more capable
solid-fuelled Minuteman ICBMs replaced the last Atlas missiles. A number of
these decommissioned Atlas ICBMs were refurbished for use by the Air Force
and the National Aeronautics and Space Administration (NASA) as satellite
launch vehicles; the last refurbished Atlas was launched from Vandenberg
AFB with a military meteorology satellite in 1995.
NASA
ordered a number of “man-rated” (modified with safety features to carry
humans) Atlas D models-designated as the Atlas LV-3B-for the orbital
flights of its first human spaceflight program, Project Mercury. Astronaut
John H. Glenn, Jr. became the first American to orbit the Earth in his
Friendship 7 Mercury capsule launched atop an Atlas LV-3B on February 20,
1962, followed by astronauts Carpenter, Schirra and Cooper in 1962 and
1963.

Scott Carpenter's Aurora 7 Mercury Atlas rocket lifts off from Cape
Canaveral, Florida, on May 24, 1962.
The
Atlas space launch vehicle has been regularly upgraded since its
introduction, including a longer tank, improved rocket engines, and
enhanced electronics and computer systems, enabling the rocket to carry
larger and heavier payloads. Atlas vehicles, equipped with a variety of
upper stages such as the Burner II, Agena and Centaur, have launched a
wide variety of military, scientific, and commercial spacecraft for more
than four decades, including the Surveyor lunar landers, the Pioneer 10
and 11 planetary probes to Jupiter and Saturn, and the Pioneer Venus
mission.
The last
of the “basic” Atlas versions, the Atlas 2A and 2AS, built by Lockheed
Martin (which acquired the Convair division of General Dynamics) and
equipped with a Centaur upper stage, can carry large payloads, such as
communications satellites, weighing almost 8,500 pounds (3,856 kilograms)
to a geostationary orbit, 22,300 miles (35,888 kilometres) above the
Equator. The Atlas 3, introduced in 2000, eliminates the booster engine
stage, replacing it and the sustainer engine with a pair of powerful,
Russian-built RD-180 rocket engines that can be throttled up and down to
adjust for aerodynamic stresses during ascent-an ironic twist for a
vehicle originally designed to launch nuclear warheads against the former
Soviet Union.

Atlas Agena target vehicle lift-off
for Gemini 11 from Pad 14 at Kennedy Space Centre, 1966.
Once the Agena was in orbit, Gemini 11 rendezvoused and docked with it.
More
than 50 years after its conception, the Atlas continues to evolve. The
summer of 2002, will see the first launch of the Atlas 5, a robust vehicle
that will be capable of lifting more than 19,000 pounds (8,618 kilograms)
to a geostationary transfer orbit. Like a fine wine, the legendary Atlas
just keeps getting better with age.
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