All About the Space Shuttle
By Marty McDowell/NASA
Space Shuttles are the main element of America's Space Transportation
System and are used for space research and space applications. The
shuttles are the first vehicles capable of being launched into space and
returning to earth on a routine basis.
Space shuttles are used as orbiting laboratories in which scientists
and mission specialists conduct a wide variety of scientific experiments,
and study and photograph stars, galaxies, the planets, and other bodies in
and beyond the universe.
Crews aboard space shuttles place satellites in orbit. They also
rendezvous with satellites to carry out repairs and return them to orbit.
Satellites are also returned to earth in space shuttles for refurbishment
A True Aerospace Vehicle
The space shuttles are true aerospace vehicles. They leave earth and
its atmosphere under rocket power provided by three liquid-fueled main
engines and two solid-fuel boosters attached to an external liquid fuel
After their missions in orbit end, the shuttles streak back through the
atmosphere and are maneuvered to land like an airplane. The shuttles,
however, are without power and they land on runways like a glider.
Other rockets can place heavy payloads into space, but they are used
only once. Space shuttles are designed to be used 100 times.
Space shuttles are used to transport complete scientific laboratories
into space. The laboratories remain inside the payload bay throughout the
mission. They are removed after the orbiter returns to earth and can be
prepared for another flight.
Some of these laboratories, like the Spacelab developed by the European
Space Agency, provide facilities for several specialists to conduct
experiments in such fields as medicine, astronomy, and materials
Among the types of satellites the shuttle can orbit and service in
space are those involved in environmental and resources protection,
weather forecasting, navigation, oceanographic studies, and other fields
useful to citizens throughout the world.
Interplanetary spacecraft can be placed into orbit by space shuttles
with the use of a propulsion unit called the Inertial Upper Stage (IUS).
After the satellite or spacecraft is deployed from the shuttle payload
bay, the IUS is ignited to accelerate the spacecraft deep into space. The
IUS is also used to boost satellites into an orbit higher than the space
shuttle's maximum altitude of 600 miles.
In the future, space shuttles will be used to carry into orbit the
structural components that will be assembled and become the space station,
a permanent facility in which crews of astronauts will work for extended
periods of time in space. The space station will have its own solar power
units and astronauts will carry out a wide range of scientific activities.
Space shuttles will not only be used to help construct the space station,
but will be used to ferry crew members and supplies between it and earth.
In 1969, shortly after the first moon landing of the Apollo program,
the President's Space Task Group recommended that the United States
initiate a program to develop a new space transportation system. In 1970
NASA initiated engineering, design, and cost studies dealing with the
concept of a reusable manned spacecraft that utilized strap-on solid
propellant rockets and an expendable liquid fuel/oxidizer tank.
On January 5, 1972, President Richard M. Nixon gave NASA authority to
proceed with development of this type of reusable space system. NASA
selected the Space Transportation Systems Division of Rockwell
International, Downey, Calif., to build the orbiters. Rockwell's
Rocketdyne Division builds the three main engines used on each orbiter.
Morton Thiokol, Brigham City, Utah, makes the solid rocket booster motors,
and Martin Marietta Corp., New Orleans, La., makes the external fuel tank.
There is more about the history
of the Space Shuttle in the 1970s here.
The space shuttle system is composed of several large components: the
orbiter, the main engines, the external tank , and solid rocket boosters.
The gross launch weight is about 4.5 million pounds (varies based on
payload weight and consumable supplies).
Orbiter: Each orbiter is 121 feet long, has a wingspan of 78
feet, and a height of 57 feet. It is about the size of a DC-9 commercial
airliner, and can carry a payload of 65,000 pounds into space. The payload
bay is 60 feet long and 15 feet in diameter. The landing weight will vary
from mission to mission and ranges from 200,000 pounds to 230,000 pounds.
Most of its basic construction, like an aircraft, is of aluminum. The
forward fuselage houses the cockpit and crew cabin and crew work areas.
The mid-fuselage area consists of the payload bay, and the wing and main
landing gear attach points. The aft fuselage houses the main engines, the
orbital maneuvering system, the reaction control system pods, the wing aft
spar, and the attach point for the vertical tail. Each orbiter is designed
with a lifetime of about 100 space missions.
Main Engines: Each main engine, operating on a mixture of liquid
oxygen and liquid hydrogen, produces a sea level thrust of 375,000 pounds
and a vacuum thrust of 470,000 pounds. They can be throttled over a thrust
range of 65 to 109 percent, allowing a high power setting during liftoff
and initial ascent, but a power reduction to limit acceleration of the
orbiter to 3Gs during final ascent. The engines are gimbaled (movable) to
provide pitch, yaw, and roll control during ascent phases of flight.
Normal engine operating time on each flight is about 8.5 minutes. Each
engine has a designed lifetime of about 7.5 operating hours.
External Tank: Each external tank is 154 feet long and 28.6 feet
in diameter. They are constructed primarily of aluminum alloys. Empty
weight of an external tank is 78,100 pounds. When filled and flight ready,
each has a gross weight of 1,667,677 pounds and contains nearly 1.6
million pounds (143,060 gallons) of liquid oxygen and more than 226,000
pounds (526,126 gallons) of liquid hydrogen. The external tank is the only
major part of the space shuttle system not reused after each flight.
Solid Rocket Boosters: The space shuttle solid
rocket boosters (SRB) are the largest solid propellant motors ever
built and the first to be used on a manned spacecraft. Each motor is made
of 11 individual weld-free steel segments joined together with
high-strength steel pins. Each assembled motor is 116 feet long, 12 feet
in diameter, and contains more than l million pounds of solid propellant.
The exhaust nozzles are gimbaled to provide yaw, pitch, and roll control
to help steer the orbiter on its ascent path. The solid propellant is made
of atomized aluminum powder (fuel), ammonium perchlorate (oxidizer), iron
oxide powder (catalyst), plus a binder and curing agent. The boosters burn
for two minutes in parallel with the main engines during initial ascent
and give the added thrust needed to achieve orbital altitude. After
approximately two minutes of flight, at an altitude of about 24 miles, the
booster casings separate from the external tank. They descend by parachute
into the Atlantic Ocean where they are recovered by ship, returned to
land, and refurbished for reuse.
Orbital Maneuvering System (OMS): Two rocket units at the
orbiter's aft end, at the base of the vertical tail, are used to place the
vehicle onto its final orbital path and they are used for extended
maneuvering while in space. The OMS is also used to slow the vehicle's
speed in orbit at the end of the mission. When the orbiter slows down,
gravity begins pulling it back into the atmosphere and it glides back to
earth for a runway landing. The OMS uses nitrogen tetroxide and monomethyl
hydrazine for fuel. Each engine produces 6,000 pounds of thrust.
Reaction Control System (RCS): This system consists of 44
nozzles on both sides of the nose and each side of the aft fuselage pod
near each OMS engine. The RCS is used throughout the mission to move or
roll the orbiter as the crew carries out tasks which require the vehicle
to be pointed certain ways for experiments or photography. The RCS uses
the same types of fuel as the OMS. Thirty-eight of the thrusters produce
870 pounds of thrust each. The six others each produce 25 pounds of
Electrical Power: Three fuel cells supply electrical power on
the orbiter during all phases of a mission. The units are located in the
mid-body area of the payload bay. Electrical power is produced by the
chemical reaction of hydrogen and oxygen, which are supplied continuously
as needed to meet output requirements. A by-product of this reaction is
drinking water used by crew. Each fuel cell is connected to one of three
independent electrical distribution systems. During peak and average power
loads, all three systems are used. During minimum loads, only two are used
and the third is on standby, but can be brought back on line instantly if
needed. The system provides up to 24 kilowatts of power, ranging from 27.5
to 32.5 volts of direct current.
Hydraulic Power: Three auxiliary power units (APU) furnish power
to operate hydraulic systems on the orbiters such as the main engine
gimbaling controls, the nose and main landing gear and brake systems, and
the rudder, speed brake, and elevon flight control surfaces. The APUs are
fueled by hydrazine which is changed into a hot gas by a granular
catalyst. The momentum of the expanding gas spins turbine blades and this
energy is transferred to gearboxes on the hydraulic pump units. All three
APUs operate during launch, but only two are needed for reentry and
Environment Control and Life Support System: The orbiter's
environmental control and life-support system purifies the cabin air, adds
fresh oxygen, keeps the pressure at sea level, heats and cools the air,
and provides drinking and wash water. The system also includes lavatory
facilities. The cabin is pressurized to sea level (14.7 psi) with 21
percent oxygen and 79 percent nitrogen, comparable to earth's atmosphere.
The air is circulated through lithium hydroxide/charcoal cannisters which
remove carbon dioxide. The cannisters are changed on a regular basis. Heat
from the cabin and flight-deck electronics is collected by a circulating
coolant water system and transferred to radiator panels on the payload bay
doors where it is dissipated. The fuel cells produce about seven pounds of
water each hour. It is stored in tanks, and the excess water is dumped
overboard when the tanks are full. The lavatory unit collects and
processes body waste, and also collects wash water from the personal
hygiene station. The lavatory unit, located in the mid deck area, operates
much like those on commercial airlines but is designed for a weightless
Thermal Protection: The thermal protection system is designed to
limit the temperature of the orbiter's aluminum and graphite epoxy
structures to about 350 degrees (F) during reentry. There are four types
of materials used to protect the orbiter. Reinforced carbon-carbon is a
composite of a layer of graphite cloth contained in a carbon matrix. It is
used on the nose cap and wing leading edges where temperatures exceed
2,300 degrees (F). High-temperature reusable surface insulation consists
of about 20,000 tiles located mainly on the lower surfaces of the vehicle.
They are about six inches square and made of a low-density silica fiber
insulator bonded to the surface in areas where temperatures reach up to
1,300 degrees (F). Low-temperature reusable surface insulation also
consists of tiles. There are about 7000 of this variety on the upper wing
and fuselage sides where temperatures range from 700 to 1,200 degrees (F).
Flexible reusable surface insulation (coated Nomex felt) is sheet-type
material applied directly to the payload bay doors, sides of the fuselage
and upper wing areas where heat does not exceed 700 degrees (F).