Space Shuttle program
Space Shuttle program
In its nearly 30-year history, the space shuttle program has seen exhilarating highs and devastating lows. The fleet has taken astronauts on dozens of successful missions, resulting in immeasurable scientific gains. But this success has had a serious cost. In 1986, the Challenger exploded during launch. In 2003, the Columbia broke up during re-entry over Texas. Since the Columbia accident, the shuttles have been grounded pending redesigns to improve their safety. The 2005 shuttle Discovery was supposed to initiate the return to flight, but a large piece of insulating foam broke free from its external fuel tank, leaving scientists to solve the mystery and the program grounded once more until July 2006, when the Discovery and Atlantis both carried out successful missions.
In this article, we examine the monumental technology behind America’s shuttle program, the mission it was designed to carry out, and the extraordinary efforts that NASA has made to return the shuttle to flight.
First, let’s look at the parts of the space shuttle and a typical mission.
The space shuttle consists of the following major components:
- two solid rocket boosters (SRB) – critical for the launch
- external fuel tank (ET) – carries fuel for the launch
- orbiter – carries astronauts and payload
The space shuttle flight path.
A typical shuttle mission is as follows:
- getting into orbit launch – the shuttle lifts off the launching pad ascent orbital maneuvering burn
- orbit – life in space
A typical shuttle mission lasts seven to eight days, but can extend to as much as 14 days depending upon the objectives of the mission. Let’s look at the stages of a mission one by one.
One of the space shuttle’s main engines
Launching the Space Shuttle
To lift the 4.5 million pound (2.05 million kg) shuttle from the pad to orbit (115 to 400 miles/185 to 643 km) above the Earth, the shuttle uses the following components:
- two solid rocket boosters (SRB)
- three main engines of the orbiter
- the external fuel tank (ET)
- orbital maneuvering system (OMS) on the orbiter
Let’s look at these components closely.
Solid Rocket Boosters
The SRBs are solid rockets that provide most of the main force or thrust (71 percent) needed to lift the space shuttle off the launch pad. In addition, the SRBs support the entire weight of the space shuttle orbiter and fuel tank on the launch pad. Each SRB has the following parts:
- solid rocket motor – case, propellant, igniter, nozzle
- solid propellant fuel – atomized aluminum (16 percent) oxidizers – ammonium perchlorate (70 percent) catalyst – iron oxide powder (0.2 percent) binder – polybutadiene acrylic acid acrylonite (12 percent) curing agent – epoxy resin (2 percent)
- jointed structure
- synthetic rubber o-rings between joints
- flight instruments
- recovery systems – parachutes (drogue, main) floatation devices signaling devices
- explosive charges for separating from the external tank
- thrust control systems
- self-destruct mechanism
Because the SRBs are solid rocket engines, once they are ignited, they cannot be shut down. Therefore, they are the last component to light at launch.
The orbiter has three main engines located in the aft (back) fuselage (body of the spacecraft). Each engine is 14 feet (4.3 m) long, 7.5 feet (2. 3 m) in diameter at its widest point (the nozzle) and weighs about 6,700 lb (3039 kg).
The main engines provide the remainder of the thrust (29 percent) to lift the shuttle off the pad and into orbit.
The engines burn liquid hydrogen and liquid oxygen, which are stored in the external fuel tank (ET), at a ratio of 6:1. They draw liquid hydrogen and oxygen from the ET at an amazing rate, equivalent to emptying a family swimming pool every 10 seconds! The fuel is partially burned in a pre-chamber to produce high pressure, hot gases that drive the turbo-pumps (fuel pumps). The fuel is then fully burned in the main combustion chamber and the exhaust gases (water vapor) leave the nozzle at approximately 6,000 mph (10,000 km/h). Each engine can generate between 375,000 and 470,000 lb (1,668,083 to 2,090,664 N) of thrust; the rate of thrust can be controlled from 65 percent to 109 percent maximum thrust. The engines are mounted on gimbals (round bearings) that control the direction of the exhaust, which controls the forward direction of the rocket
External Fuel Tank
As mentioned above, the fuel for the main engines is stored in the ET. The ET is 158 ft (48 m) long and has a diameter of 27.6 ft (8.4 m). When empty, the ET weighs 78,000 lb (35,455 kg). It holds about 1.6 million lb (719,000 kg) of propellant with a total volume of about 526,000 gallons (2 million liters).
The ET is made of aluminum and aluminum composite materials. It has two separate tanks inside, the forward tank for oxygen and the aft tank for hydrogen, separated by an intertank region. Each tank has baffles to dampen the motion of fluid inside. Fluid flows from each tank through a 17-inch (43 cm) diameter feed line out of the ET through an umbilical line into the shuttle’s main engines. Through these lines, oxygen can flow at a maximum rate of 17,600 gallons/min (66,600 l/min) and hydrogen can flow at a maximum rate of 47,400 gallons/min (179,000 l/min).
The ET is covered with a 1-inch (2.5 cm) thick layer of spray-on, polyisocyanurate foam insulation. The insulation keeps the fuels cold, protects the fuel from heat that builds up on the ET skin in flight, and minimizes ice formation. When Columbia launched in 2003, pieces of the insulating foam broke off the ET and damaged the left wing of the orbiter, which ultimately caused Columbia to break up upon re-entry.
The Trouble with O-rings
During the January 1986 launch of Challenger, the temperature was below zero. The cold shrank the rubber o-rings and they did not seal the joints properly. During ascent, hot gases escaped through one of the joints of the SRB. Like a blowtorch, the gases cut through the thin skin of the ET and ignited the liquid hydrogen fuel. Challenger broke up and the crew was lost. NASA re-designed the SRB joints, implemented new rules regarding launches in cold weather, and built a new system for the crew to escape from the shuttle during ascent.
Space Shuttle Liftoff
The two orbital maneuvering systems’ (OMS) engines are located in pods on the aft section of the orbiter, one on either side of the tail. These engines place the shuttle into final orbit, change the shuttle’s position from one orbit to another, and slow the shuttle down for re-entry.
The OMS engines burn monomethyl hydrazine fuel (CH3NHNH2) and nitrogen tetroxide oxidizer (N2O4). Interestingly, when these two substances come in contact, they ignite and burn automatically (i.e., no spark required) in the absence of oxygen. The fuel and oxidizer are kept in separate tanks, each pressurized by helium. The helium pushes the fluids through the fuel lines (i.e., no mechanical pump required). In each fuel line, there are two spring-loaded solenoid valves that close the lines. Pressurized nitrogen gas, from a small tank located near the engine, opens the valves and allows the fuel and oxidizer to flow into the combustion chamber of the engine. When the engines shut off, the nitrogen goes from the valves into the fuel lines momentarily to flush the lines of any remaining fuel and oxidizer; this purge of the line prevents any unwanted explosions. During a single flight, there is enough nitrogen to open the valves and purge the lines 10 times!
Either one or both of the OMS engines can fire, depending upon the orbital maneuver. Each OMS engine can produce 6,000 lb (26,400 N) of thrust. The OMS engines together can accelerate the shuttle by 2 ft/s2 (0.6 m/s2). This acceleration can change the shuttle’s velocity by as much as 1,000 ft/s (305 m/s). To place into orbit or to de-orbit takes about 100-500 ft/s (31-153 m/s) change in velocity. Orbital adjustments take about 2 ft/s (0.61 m/s) change in velocity. The engines can start and stop 1,000 times and have a total of 15 h burn time.
Profile of shuttle launch and ascent into orbit
As the shuttle rests on the pad fully fueled, it weighs about 4.5 million pounds or 2 million kg. The shuttle rests on the SRBs as pre-launch and final launch preparations are going on through T minus 31 seconds:
- T minus 31 s – the on-board computers take over the launch sequence.
- T minus 6.6 s – the shuttle’s main engines ignite one at a time (0.12 s apart). The engines build up to more than 90 percent of their maximum thrust.
- T minus 3 s – shuttle main engines are in lift-off position.
- T minus 0 s -the SRBs are ignited and the shuttle lifts off the pad.
- T plus 20 s – the shuttle rolls right (180 degree roll, 78 degree pitch).
- T plus 60 s – shuttle engines are at maximum throttle.
- T plus 2 min – SRBs separate from the orbiter and fuel tank at an altitude of 28 miles (45 km). Main engines continue firing. Parachutes deploy from the SRBs. SRBs will land in the ocean about 140 miles (225 km) off the coast of Florida. Ships will recover the SRBs and tow them back to Cape Canaveral for processing and re-use.
- T plus 7.7 min – main engines throttled down to keep acceleration below 3g’s so that the shuttle does not break apart.
- T plus 8.5 min – main engines shut down.
- T plus 9 min – ET separates from the orbiter. The ET will burn up upon re-entry.
- T plus 10.5 min – OMS engines fire to place you in a low orbit.
- T plus 45 min – OMS engines fire again to place you in a higher, circular orbit (about 250 miles/400 km).
You are now in outer space and ready to continue your mission.
The Space Shuttle in Orbit
Once in space, the shuttle orbiter is your home for seven to 14 days. The orbiter can be oriented so that the cargo bay doors face toward the Earth or away from the Earth depending upon the mission objectives; in fact, the orientation can be changed throughout the mission. One of the first things that the commander will do is to open the cargo bay doors to cool the orbiter.
- crew compartment – where you will live and work
- forward fuselage (upper, lower parts) – contains support equipment (fuel cells, gas tanks) for crew compartment
- forward reaction control system (RCS) module – contains forward rocket jets for turning the orbiter in various directions
- movable airlock – used for spacewalks and can be placed inside the crew compartment or inside the cargo bay
- mid-fuselage: contains essential parts (gas tanks, wiring, etc.) to connect the crew compartment with the aft engines; forms the floor of the cargo bay
- cargo bay doors – roof of the cargo bay and essential for cooling the orbiter
- remote manipulator arm – located in the cargo bay: moves large pieces of equipment in and out of the cargo bay; platform for spacewalking astronauts
- aft fuselage – contains the main engines
- OMS/RCS pods (2) – contain the orbital maneuvering engines and the aft RCS module; turn the orbiter and change orbits
- airplane parts of the orbiter – fly the shuttle upon landing (wings, tail, body flap)
You will live in the crew compartment, which is located in the forward fuselage. The crew compartment has 2,325 cu.ft of space with the airlock inside or 2,625 cu.ft with the airlock outside.
The crew compartment has three decks:
flight deck – uppermost deck
- forward deck – contains all of the controls and warning systems for the space shuttle (also known as the cockpit)
- seats – commander, pilot, specialist seats (two)
- aft deck – contains controls for orbital operations: maneuvering the orbiter while in orbit (rendezvous, docking, deploying payload, and working the remote manipulator arm
- living quarters (galley, sleeping bunks, toilet)
- stowage compartments (personal gear, mission-essential equipment, experiments)
- exercise equipment
- airlock – on some flights
- entry hatch
lower deck (equipment bay) – contains life support equipment, electrical systems, etc. Now that you have seen the parts of the orbiter, let’s look closely at how the orbiter lets you live in space.
The shuttle orbiter provides an environment where you can live and work in space.
Space shuttle Endeavour (STS113) in orbit as seen from the International Space Station.
It must be able to do the following:
- provide life support – everything the Earth does for us (atmosphere control, supply and recycling;water; temperature control; light; food supply; waste removal; fire protection)
- change position and change orbits
- let you talk with ground-based flight controllers (communications and tracking)
- find its way around (navigation)
- make electrical power
- coordinate and handle information (computers)
- enable you to do useful work (launch/retrieve satellites; construction – such as building the International Space Station; conduct experiments)
Life Aboard the Space Shuttle
The orbiter must provide you with an environment similar to Earth. You must have air, food, water, and a comfortable temperature. The orbiter must also take away the wastes that your body produces (carbon dioxide, urine, feces) and protect you from fire. Let’s look at these various aspects of the orbiter’s life support system.
On board the space shuttle, you need to have the following:
- atmosphere similar to Earth
- carbon dioxide removed
- contaminating or trace gases removed
- normal humid environment
Our atmosphere is a mixture of gases (78 percent nitrogen, 21 percent oxygen, 1 percent other gases) at a pressure of 14 lbs/in2 (1 atm) that we breathe in and out. The space shuttle must provide a similar atmosphere. To do this, the orbiter carries liquid oxygen and liquid nitrogen in two systems of pressurized tanks, which are located in the mid-fuselage (each system has two tanks for a total of four tanks). The cabin pressurization system combines the gases in the correct mixture at normal atmospheric pressure. While in orbit, only one oxygen-nitrogen system is used to pressurize the orbiter. During launch and landing, both systems of each gas are used.
Five loops of fans circulate the atmosphere. The circulated air picks up carbon dioxide, heat and moisture:
- Chemical carbon dioxide canisters remove carbon dioxide by reacting it with lithium hydroxide. These canisters are located in the lower deck of the crew compartment and changed every 12 hours.
- Filters and charcoal canisters remove trace odors, dust and volatile chemicals from leaks, spills and outgassing.
- A cabin heat exchanger in the lower deck cools the air and condenses the moisture, which collects in a slurper. Water from the slurper is moved with air to a fan separator, which uses centrifugal force to separate water from air. The air is recirculated and the water goes to a wastewater tank.
Besides air, water is the most important quantity aboard the orbiter. Water is made from liquid oxygen and hydrogen in the space shuttle’s fuel cells (the fuel cells can make 25 lb (11 kg) of water per hour). The water passes through a hydrogen separator to eliminate any trapped hydrogen gas (excess hydrogen gas is dumped overboard). The water is then stored in four water storage tanks located in the lower deck. Each tank can hold 165 lb (75 kg). The water tanks are pressurized by nitrogen so that water can flow to the mid-deck for use by the crew. Drinkable water is then filtered to remove microbes and can be warmed or chilled through various heat exchangers depending upon the use (food preparation, consumption, personal hygiene). Excess water produced by the fuel cells gets routed to a wastewater tank and subsequently dumped overboard.
Outer space is an extremely cold environment and temperatures will vary drastically in different parts of the orbiter. You might think that heating the orbiter would be a problem. However, the electronic equipment generates more than enough heat for the ship. The problem is getting rid of the excess heat. So the temperature control system has to carry out two major functions:
- Distribute heat where it is needed on the orbiter (mid-fuselage and aft sections) so that vital systems do not freeze in the cold of space.
- Get rid of the excess heat.
To do this, the shuttle has two methods to handle temperature control:
- Passive methods – generally simple, handle small heat loads and require little maintenance Insulating materials (blankets), surface coatings, paints – reduce heat loss through the walls of the various components just like your home insulation. Electrical heaters – use electrically-heated wires like a toaster to heat various areas.
- Active methods – more complex, use fluid to handle large heat loads, require maintenance Cold plates – metal plates that collect heat by direct contact with equipment or conduction Heat exchangers – collect heat from equipment using fluid. The equipment radiates heat to a fluid (water, ammonia) which in turn passes heat on to freon. Both fluids are pumped and recirculated to remove heat. Pumps, lines, valves – transport the collected heat from one area to another. Radiators – located on the inside surfaces of the cargo bay doors that radiate the collected heat to outer space Flash evaporator/ammonia boilers – these devices are located in the aft fuselage and transfer heat from Freon coolant loops overboard when cargo bay doors are closed or when cargo bay radiators are overloaded. Flash evaporator Freon coolant loops wrap around an inner core. The evaporator sprays water on the heated core. The water evaporates removing heat. The water vapor is vented overboard. Ammonia boiler Freon coolant loops pass through a tank of pressurized ammonia. Heat released from the freon causes the ammonia to boil. Ammonia vapor is dumped overboard.
The cabin heat exchanger also controls the cabin temperature. It circulates cool water to remove excess heat (cabin air is also used to cool electronic equipment) and transfers this heat to a Freon exchanger. The Freon then transfers the heat to other orbiter systems (e.g., cryogenic gas tanks, hydraulic systems) and radiates excess heat to outer space.
The orbiter has internal fluorescent floodlights that illuminate the crew compartment. The orbiter has external floodlights to illuminate the cargo bay. Finally, the control panels are lighted internally for easy viewing.
Food is stored on the mid-deck of the crew compartment. Food comes in several forms (dehydrated, low moisture, heat-stabilized, irradiated, natural and fresh). The orbiter has a galley-style kitchen module along the wall next to the entry hatch, which is equipped with the following:
- food storage compartments
- food warmers
- a food preparation area with warm and cold water outlets
- metal trays so the food packages and utensils do not float away
Like any home, the orbiter must be kept clean, especially in space when floating dirt and debris could present a hazard. Wastes are made from cleaning, eating, work and personal hygiene. For general housecleaning, various wipes (wet, dry, fabric, detergent and disinfectant), detergents, and wet/dry vacuum cleaners are used to clean surfaces, filters and the astronauts. Trash is separated into wet trash bags and dry trash bags, and the wet trash is placed in an evaporator that will remove the water. All trash bags are stowed in the lower deck to be returned to Earth for disposal. Solid waste from the toilet is compacted, dried and stored in bags where it is returned to Earth for disposal (burning). Liquid waste from the toilet goes to the wastewater tank where it is dumped overboard.
Fire is one of the most dangerous hazards in space. The orbiter has a Fire Detection and Suppression Subsystem that consists of the following:
- area smoke detectors on each deck
- smoke detectors in each rack of electrical equipment
- alarms and warning lights in each module
- non-toxic portable fire extinguishers (carbon dioxide-based)
- personal breathing apparatus – mask and oxygen bottle for each crew member
After a fire is extinguished, the atmosphere control system will filter the air to remove particulates and toxic substances.
Space Shuttle Positioning, Communication and Navigation
To change the direction that the orbiter is pointed (attitude), you must use the reaction control system (RCS) located on the nose and OMS pods of the aft fuselage.
The RCS has 14 jets that can move the orbiter along each axis of rotation (pitch, roll, yaw). The RCS thrusters burn monomethyl hydrazine fuel and nitrogen tetroxide oxidizer just like the OMS engines described previously. Attitude changes are required for deploying satellites or for pointing (mapping instruments, telescopes) at the Earth or stars.
To change orbits (e.g., rendezvous, docking maneuvers), you must fire the OMS engines. As described above, these engines change the velocity of the orbiter to place it in a higher or lower orbit.
Tracking and Communication
You must be able to talk with flight controllers on the ground daily for the routine operation of the mission. In addition, you must be able to communicate with each other inside the orbiter or its payload modules and when conducting spacewalks outside.
NASA’s Mission Control in Houston will send signals to a 60 ft radio antenna at White Sands Test Facility in New Mexico. White Sands will relay the signals to a pair of Tracking and Data Relay satellites in orbit 22,300 miles above the Earth. The satellites will relay the signals to the space shuttle. The system works in reverse as well.
The orbiter has two systems for communicating with the ground:
- S-band – voice, commands, telemetry and data files
- Ku-band (high bandwidth) – video and transferring two-way data files
The orbiter has several intercom plug-in audio terminal units located throughout the crew compartment. You will wear a personal communications control with a headset. The communications control is battery-powered and can be switched from intercom to transmit functions. You can either push to talk and release to listen or have a continuously open communication line. To talk with spacewalkers, the system uses a UHF frequency, which is picked up in the astronaut’s space suit.
The orbiter also has a series of internal and external video cameras to see inside and outside.
Navigation, Power and Computers
The orbiter must be able to know precisely where it is in space, where other objects are and how to change orbit. To know where it is and how fast it is moving, the orbiter uses global positioning systems (GPS). To know which way it is pointing (attitude), the orbiter has several gyroscopes. All of this information is fed into the flight computers for rendezvous and docking maneuvers, which are controlled in the aft station of the flight deck.
All of the on-board systems of the orbiter require electrical power. Three fuel cells make electricity; they are located in the mid fuselage under the payload bay. These fuel cells combine oxygen and hydrogen from pressurized tanks in the mid fuselage to make electricity and water. Like a power grid on Earth, the orbiter has a distribution system to supply electrical power to various instrument bays and areas of the ship. The water is used by the crew and for cooling.
The orbiter has five on-board computers that handle data processing and control critical flight systems. The computers monitor equipment and talk to each other and vote to settle arguments. Computers control critical adjustments especially during launch and landing:
- operations of the orbiter (housekeeping functions, payload operations, rendezvous/docking)
- interface with the crew
- caution and warning systems
- data acquisition and processing from experiments
- flight maneuvers
Pilots essentially fly the computers, which fly the shuttle. To make this easier, the shuttles have a Multifunctional Electronic Display Subsystem (MEDS), which is a new, full color, flat, 11-panel display system. The MEDS, also known as the “glass cockpit”, provides graphic portrayals of key light indicators (attitude, altitude, speed). The MEDS panels are easy to read and make it easier for shuttle pilots to interact with the orbiter.
The glass cockpit
Work Aboard the Shuttle
The shuttle was designed to deploy and retrieve satellites as well as deliver payloads to Earth orbit. To do this, the shuttle uses the Remote Manipulator System (RMS). The RMS was built by Canada and is a long arm with an elbow and wrist joint. You can control the RMS from the aft flight deck. The RMS can grab payloads (satellites) from the cargo bay and deploy them, or grab on to payloads and place them into the bay.
In the past, the shuttle was used for delivering satellites and conducting experiments in space. Within the mid-deck, there are racks of experiments to be conducted during each mission. When more space was needed, the mission used the Spacelab module, which was built by the European Space Agency (ESA). It fit into the cargo bay and was accessed by a tunnel from the mid-deck of the crew compartment. It provided a “shirt-sleeve” environment in which you could work. The Spacelab was lost along with Columbia in 2003. Now, most experiments will be conducted aboard the International Space Station (ESA is building a new science module called Columbus for the ISS).
The shuttle’s major role is building and resupplying the International Space Station. The shuttle delivers components built on Earth. Astronauts use the RMS to remove components from the cargo bay and to help attach them to existing modules in space station.
Astronauts install a truss, which was delivered to the space station by Endeavour (STS113).
You will spend most of your time on the shuttle doing work to accomplish the mission objectives. Besides work, you must exercise frequently on the treadmill to counteract the loss of bone and muscle mass associated with weightlessness. You will also eat at the galley and sleep in your bunk-style sleeping quarters. You will have a toilet and personal hygiene facilities for use. You may have to perform spacewalks to accomplish the mission objectives. This will involve getting into a space suit and going through depressurization procedures in the airlock.
When your mission objectives have been accomplished, it will be time to return to Earth. Let’s look at this process in the next section.
The Shuttle’s Return to Earth
For a successful return to Earth and landing, dozens of things have to go just right.
First, the orbiter must be maneuvered into the proper position. This is crucial to a safe landing.
When a mission is finished and the shuttle is halfway around the world from the landing site (Kennedy Space Center, Edwards Air Force Base), mission control gives the command to come home, which prompts the crew to:
- Close the cargo bay doors. In most cases, they have been flying nose-first and upside down, so they then fire the RCS thrusters to turn the orbiter tail first.
- Once the orbiter is tail first, the crew fires the OMS engines to slow the orbiter down and fall back to Earth; it will take about 25 minutes before the shuttle reaches the upper atmosphere.
- During that time, the crew fires the RCS thrusters to pitch the orbiter over so that the bottom of the orbiter faces the atmosphere (about 40 degrees) and they are moving nose first again.
- Finally, they burn leftover fuel from the forward RCS as a safety precaution because this area encounters the highest heat of re-entry.
Because it is moving at about 17,000 mph (28,000 km/h), the orbiter hits air molecules and builds up heat from friction (approximately 3000 degrees F, or 1650 degrees C). The orbiter is covered with ceramic insulating materials designed to protect it from this heat. The materials include:
- Reinforced carbon-carbon (RCC) on the wing surfaces and underside
- High-temperature black surface insulation tiles on the upper forward fuselage and around the windows
- White Nomex blankets on the upper payload bay doors, portions of the upper wing and mid/aft fuselage
- Low-temperature white surface tiles on the remaining areas
Maneuvering of the orbiter for re-entry
These materials are designed to absorb large quantities of heat without increasing their temperature very much. In other words, they have a high heat capacity. During re-entry, the aft steering jets help to keep the orbiter at its 40 degree attitude. The hot ionized gases of the atmosphere that surround the orbiter prevent radio communication with the ground for about 12 minutes (i.e., ionization blackout).
When re-entry is successful, the orbiter encounters the main air of the atmosphere and is able to fly like an airplane. The orbiter is designed from a lifting body design with swept back “delta” wings. With this design, the orbiter can generate lift with a small wing area. At this point, flight computers fly the orbiter. The orbiter makes a series of S-shaped, banking turns to slow its descent speed as it begins its final approach to the runway. The commander picks up a radio beacon from the runway (Tactical Air Navigation System) when the orbiter is about 140 miles (225 km) away from the landing site and 150,000 feet (45,700 m) high. At 25 miles (40 km) out, the shuttle’s landing computers give up control to the commander. The commander flies the shuttle around an imaginary cylinder (18,000 feet or 5,500 m in diameter) to line the orbiter up with the runway and drop the altitude. During the final approach, the commander steepens the angle of descent to minus 20 degrees (almost seven times steeper than the descent of a commercial airliner).
Shuttle flight path for landing
When the orbiter is 2,000 ft (610 m) above the ground, the commander pulls up the nose to slow the rate of descent. The pilot deploys the landing gear and the orbiter touches down. The commander brakes the orbiter and the speed brake on the vertical tail opens up. A parachute is deployed from the back to help stop the orbiter. The parachute and the speed brake on the tail increase the drag on the orbiter. The orbiter stops about midway to three-quarters of the way down the runway.
Space shuttle orbiter touching down
After landing, the crew goes through the shutdown procedures to power down the spacecraft. This process takes about 20 minutes. During this time, the orbiter is cooling and noxious gases, which were made during the heat of re-entry, blow away. Once the orbiter is powered down, the crew exits the vehicle. Ground crews are on-hand to begin servicing the orbiter.
Orbiter being serviced just after landing
20 Aug, 2013
Space Shuttle program
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