Space Shuttle - astronomy.
Publié le 11/05/2013
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The two SRBs, with their combined thrust of some 26 million newtons (about 5.8 million lb), provide most of the power for the first two minutes of flight.
The SRBs takethe space shuttle to an altitude of 45 km (28 mi) and a speed of 4,973 km/h (3,094 mph) before they separate and fall back into the ocean to be retrieved,refurbished, and prepared for another flight.
After the boosters fall away, the three main engines continue to provide thrust.
These engines are clustered at the rear end of the orbiter and have a combined thrustof almost 5.3 million newtons (almost 1.2 million lb).
The space shuttle's liquid-propellant engines are the world's first reusable rocket engines.
They fire for only eightminutes for each flight, just until the shuttle reaches orbit, and are designed to operate for 55 flights.
The engines are very large—4.2 m (14 ft) long, and 2.4 m (8 ft)in diameter at the wide end of the cone-shaped nozzle at the rear of the orbiter.
Another propulsion system takes over once the space shuttle's main engines shut down as the ship approaches the altitude at which it will begin orbiting around Earth,known as the orbital insertion point.
Two orbital maneuvering system (OMS) engines, mounted on either side of the aft fuselage, provide thrust for major orbitalchanges.
For more exacting maneuvers in orbit, 44 small rocket engines (known as the reaction control system), clustered on the shuttle's nose and on either side ofthe tail, are used.
They have proven indispensable in performing the shuttle's important work of retrieving, launching, and repairing satellites in orbit.
C External Fuel Tank
The giant, cylindrical, external fuel tank, with a length of 47 m (154 ft) and a diameter of 8.4 m (27.5 ft), is the largest single piece of the space shuttle.
It fuels theorbiter's three main engines.
During launch, the external tank also acts as a support for the orbiter and SRBs to which it is attached.
Inside separate pressurized tanks, the external tank holds the liquid hydrogen fuel and liquid oxygen oxidizer (which reacts with the hydrogen to produce combustion)that runs the shuttle's three main engines.
During launch, the external tank feeds the fuel under pressure through small ducts that branch off into smaller lines thatfeed directly into the main engines.
Some 450 kg (1,000 lb) of fuel are consumed by each of the main engines each second.
The space shuttle’s external fuel tank is the only part of the launch vehicle that currently is not reused.
After its 1.99 million liters (526,000 gallons) of fuel areconsumed during the first 8.5 minutes of flight, the external tank is jettisoned from the orbiter and breaks up in the upper atmosphere, its pieces falling into remoteocean waters.
During the first 17 years of shuttle flights, the external fuel tanks were made of aluminum alloys.
The tanks that the first five shuttle missions used weighed about35,000 kg (about 77,000 lb) when empty.
A design change in 1983 reduced the weight to 30,000 kg (66,000 lb) when empty.
In 1998, anticipating the extra powerthat the shuttle will need to get to the International Space Station (ISS), which will orbit at a higher altitude than the space shuttle usually uses, NASA announced theintroduction of a new tank design.
The new tanks, first used in May 1998, are made of aluminum lithium, which is significantly lighter than the aluminum alloys used forprevious tanks.
The new tanks weigh about 27,000 kg (about 59,000 lb) when empty.
III EARLY MISSIONS
In its first five years, the earliest space-shuttle missions made significant contributions, beginning with the first orbital flight tests of the Columbia orbiter in April 1981;the first launch of the second orbiter (Challenger) in April 1983; the first flight of Spacelab, with 71 scientific experiments from the United States and Europeancountries, in November 1983; the first repair of a satellite in orbit (the Solar Maximum Satellite) in April 1984; the first retrieval of satellites from orbit (Palapa andWestar) and their return to the Earth in November 1984; and the first manually assisted launch of a satellite (Syncon IV-3) from space, after retrieval and repair in orbitof the satellite Leasat in August 1985.
The shuttle program was suspended for nearly three years for evaluation and modification following the explosion of the spaceshuttle Challenger in January 1986.
IV CHALLENGER DISASTER
On January 28, 1986, Challenger and its crew were destroyed shortly after launch.
The failure of an O-ring seal of a joint on one of the SRBs was the primary cause ofthe Challenger loss.
SRBs are constructed in four cylindrical sections that must be sealed together completely to prevent the escape of the intensely hot byproducts ofthe burning fuel during launch.
O-rings are rubber rings that play a crucial part in ensuring the seal.
The cold weather on the launch day made the rubber of an O-ringon the joint between the bottom two segments of the right SRB brittle, which, combined with the faulty design of the joint, allowed hot gases from the burning solidrocket fuel to escape.
The gases and flames burned through the metal holding the rocket in position.
When the rocket broke loose, it ruptured the side of the externalfuel tank, allowing the liquid hydrogen and oxygen to mix prematurely and explode.
In early February 1986, as the nation mourned the tragic loss of the seven Challenger crew members, U.S.
President Ronald Reagan announced the creation of thePresidential Commission on the Space Shuttle Challenger Accident.
Chaired by William P.
Rogers, former secretary of state, it became known as the Rogers Commission.NASA's Challenger Data and Design Analysis Task Force also was established at this time to support the work of the Rogers Commission.
More than 6,000 people were involved in the commission's four-month investigation of the accident, and some 15,000 transcript pages were taken during public andclosed hearings.
The commission's report was published and delivered to the president on June 6, 1986.
Its recommendations included modifications of hardware andNASA procedures.
During the period when the space shuttle fleet was grounded, hundreds of major and minor modifications (many of which were planned before the accident) wereincorporated into the shuttle system.
The SRBs were completely redesigned, and a new joint design passed stringent examination and review.
The main space shuttle engines underwent the most aggressive ground-testing program in their history, equivalent in operational time to more than 36 missions.
Allengine improvements were certified to demonstrate improved reliability and operating safety margins, and they were incorporated into the engines used on theDiscovery, Columbia, Atlantis, and Endeavour orbiters.
NASA safety programs were completely reorganized as a result of another Rogers Commission recommendation.
The Office of Safety, Reliability, Maintainability, andQuality Assurance was established in 1986, and it now has direct authority for safety and related quality controls for all NASA operations.
Today, more people areassigned to safety and related programs, improved communications have been initiated, and the review system for compliance to new procedures is rigorous and well-defined.
The new Office of Safety ensures that the highest levels of NASA's management team are aware of safety issues.
V LATER MISSIONS
After the Challenger accident in 1986, more than 80 shuttle missions were completed with no serious mishaps.
The most notable of these were the scientific missionsthat launched these exploratory spacecraft: Magellan (launched May 1989), the probe designed for radar mapping of the planet Venus; Galileo (launched October1989), the unpiloted spacecraft that reached Jupiter in December 1995; Ulysses (launched October 1990), a probe designed for study of the Sun; and the Hubble.
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