solid
rocket propellants
There
are two basic kinds of propellants for missiles and rockets: liquid and
solid propellants. They each have their advantages and disadvantages.
Liquid propellants require complicated piping and pumping equipment to
feed their engines. They can provide greater propulsive thrust and
throttle their power, but take time to build up this thrust when first
ignited. Solids do not require complicated engines or plumbing, but rely
on sophisticated chemistry and strong casings to withstand the intense
pressures that they generate. They can fire much faster, and accelerate
more quickly at lift-off, but cannot be throttled in flight.

They sounded more like fireworks
than rockets but the Chinese used rockets in battle.
The very
first rockets, built by the Chinese at some unknown period in the first
millennium, used solid propellants, a variant of black powder used in
early guns. The pace of technological progress in solid propellants—and
explosives in general—was extremely slow. In fact, the rockets that
Francis Scott Key observed during the War of 1812, called Congreve rockets
after their English inventor William Congreve, and which are mentioned in
the U.S. national anthem, were virtually identical to those fired by the
Chinese eight centuries before. It was not until the middle of the 20th
century that solid propellants for rockets made a sudden and dramatic leap
forward.
Early
propellants, despite their sparks and bluster, were relatively weak.
Rockets were primarily sloppy bombardment weapons, far less effective than
a cannonball. Their poor performance prompted rocketry pioneers like
Robert Goddard to develop liquid propellants, starting first with
gasoline, then moving to kerosene and alcohol. Solid propellant rockets
still had utility, but most rocket engineers during the 1930s and 1940s
focused upon liquid fuels and oxidizers. Solids were used for many
military applications, such as short-range rockets, but they were not used
for any long-range applications, and certainly not for spaceflight due to
their comparative lack of power.
Despite
this, solid propellants were extremely attractive for military missile use
primarily because they were storable. The first liquid-fuelled ballistic
missiles like the German V-2, the American Atlas, Thor and Jupiter, and
the Russian R-7, all had to be filled with fuel and oxidizer before they
could be fired, a process that could take many hours and could be
extremely hazardous. Liquid fuels also required complex and expensive
ground handling equipment, meaning that any missile base would be
expensive and “soft”—i.e., easily damaged in an attack. Solid fuels were a
possible solution.
During
the 1940s, researchers at the Jet Propulsion Laboratory in Pasadena,
California, began working on “castable” solid propellants, which got their
name from the fact that they could be cast into moulds. John Parsons
developed asphalt as a fuel and binder (the substance that holds all the
chemicals together) together with potassium perchlorate as an oxidizer. By
the 1950s, synthetic polymers replaced the asphalt. But a major
improvement came when the rocket designers and chemists added aluminium
powder to the mix, which increased the performance of the propellant
substantially. In addition to the propellant chemistry, another major
development has been lightweight, very strong metal and composite
(including fibreglass) material casings to withstand the intense pressures
of the burning propellant.
During
the 1950s, the U.S. Air Force and the U.S. Navy cooperated with each other
to a surprising degree to develop these more powerful solid propellants.
The Navy wanted solid propellant missiles for use aboard its submarines,
where sloshing liquid fuels were a major safety risk. U.S. Air Force
leaders wanted them for a mobile intercontinental ballistic missile (ICBM)
that would be Shuttled around the countryside on railroad cars.

Static test firing for Solid
Rocket Booster.
The
first successful solid propellant ballistic missile was the U.S. Navy's
Polaris A1 submarine-launched missile, which became operational in 1960.
It had a range of 1,200 nautical miles (3,704 kilometres) and carried a
nuclear warhead. It could actually be fired from underwater, which
decreased the vulnerability of the submarine to attack. The Polaris A1 was
soon followed by upgraded versions with increased range and was eventually
replaced in the 1970s by the Poseidon missile, itself replaced by the
Trident, which is still in use today in an upgraded form.
The
first Air Force solid propellant ballistic missile was the Minuteman, so
named because it could be ready to fire on a minute's notice and did not
need to be fuelled before launch. Plans for launching the Minuteman from
railroad cars were cancelled in the early 1960s and the missiles were
instead based in underground holes called silos. Because these missiles
did not have to be pumped full of fuel and oxidizer before flight, very
little equipment was required to support them, and they could be encased
in very thick concrete to protect them from the force of a nearby nuclear
blast. The Minuteman silos were subsequently much cheaper to build than
those required for the Atlas ICBM that Minuteman replaced. Later versions
of the Minuteman still serve today, along with an even larger American
ICBM called the Peacekeeper.
Solid
rockets were also adapted for space launch missions. The first American
solid propellant rocket was the Scout, which launched relatively small
payloads into orbit. Today, the air-launched Pegasus and the
ground-launched Taurus also use solid propellants, and Italy is developing
its own solid fuel rocket. Generally solid fuelled rockets are used for
smaller satellites.

The Scout launch vehicle was used for unmanned small satellite missions,
high-altitude probes and re-entry experiments. Scout, the smallest of the
basic launch vehicles,
was the only United States' launch vehicle fuelled exclusively with solid
propellants.
Solid
rockets also became a way of boosting another rocket's performance. The
Air Force added small solid boosters to its Thor rocket to increase its
lifting capacity. NASA soon adopted this for the Delta rocket, a variant
of the Thor. A major development in solid propellant rocketry came in the
early 1960s, when United Technology Corporation (UTC) developed the
segmented booster (aerospace companies Aerojet and Thiokol also developed
segmented boosters). The motor was built in segments that could be
transported separately to the launch site and then assembled. UTC built
segmented Solid Rocket Motors (SRMs) with a 156-inch diameter for the
Titan III space launch vehicle. Later, Morton Thiokol built even larger
segmented boosters for the Space Shuttle (where they are called Solid
Rocket Boosters, or SRBs). However, the segments could allow hot gasses to
escape from the propellant casing, which is what happened in 1986 when the
Space Shuttle Challenger exploded. The National Aeronautics and Space
Administration (NASA) and the Air Force explored even larger SRBs during
the 1960s, but their size would have made them difficult to transport and
handle, and they were abandoned.
Although
the Soviet Union had gained an important early advantage over the United
States in the development of globe-spanning ICBMs, it quickly lost its
advantage. The liquid-fuelled R-7 that stunned the world by launching
Sputnik in October 1957 and later launched Yuri Gagarin into orbit proved
to be an atrocious weapon. Only a handful of them ever became operational
as ICBMs. Soviet rocket designers produced better liquid propellants than
their early ones that could be stored inside the missile for long periods
of time, but they lagged far behind the United States in solid propellant
technology.
The
Soviet Union followed the American development of solids by about a
decade, fielding their first practical solid ICBMs, known as the RT-2, in
December 1971. The Soviets were slow to eliminate liquid-propellant ICBMs
from their arsenal, probably because of the unreliability and poor
performance of their solid propellants, and did not deploy large numbers
of solid-propellant ICBMs until the 1980s. Amazingly, they even continued
using liquids on their submarines well into the 1980s, despite the fact
that these were dangerous and caused several fatal submarine sinkings. The
Soviet Union also never adopted solid rocket boosters for their space
rockets like the Americans, preferring liquid boosters instead.
Other
countries have also adopted solid propellants for their missile and space
programs. France developed the SSBS (Sol-Sol-Ballistique-Stratégique)
medium-range ballistic missile using solid propellants. Later the European
company Arianespace adopted solid boosters for the Ariane 3 and 4 space
rockets and developed large SRBs for the Ariane 5 heavy lift rocket. China
continued to use liquid-fuelled ICBMs into the 21st century, but by the
late 1990s had started tests of a new solid-fuelled ICBM. Large solid
propellant rockets remain a very difficult technology, which explains why
countries developing ballistic missile and space capabilities still use
liquid fuels. India, Iraq, Iran and North Korea all use liquid-fuelled
designs for their budding missile and rocket programs.
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