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1. Skylon Spaceplane, UK The Spacecraft of Tomorrow
2. Introduction Skylon is a design for a single-stage-to-orbit
spacepalne by the British company Reaction Engines Limited (REL),
using SABRE, a combined-cycle, air-breathing rocket propulsion
system, potentially reusable for 200 flights. The vehicle design is
for a hydrogen-fuelled aircraft that would take off from a
conventional runway, and accelerate to Mach 5.4 at 26 km (16 mi)
altitude using the atmosphere before switching the engines to use
the internal liquid oxygen(LOX) supply to take it into orbit. Once
in orbit it would release its payload of up to 15 tons. If all goes
to plan, the first test flights could happen in 2019, and Skylon
could be visiting the International Space Station by 2022. It could
carry 15 tons of cargo to a 300 km equatorial orbit on each trip,
and up to 11 tons to the International Space Station, almost 45%
more than the capacity of the European Space Agency's ATV
vehicle.
3. Synergistic Air-Breathing Rocket Engine (Sabre) The proposed
SABRE engine is not a scramjet, but a jet engine running combined
cycles of a precooled jet engine, rocket engine and ramjet. Sabre
has the unique ability to use oxygen in the air rather than from
external liquid-oxygen tanks. The Skylon could be ready to head
back to space within two days of landing. Air traveling at Mach 5
enters the engine and passes through a heat exchanger. There, a
network of paper-thin metal tubes filled with liquid helium chill
the 2,000F air to 238F almost instantly. That chilled air flows
into the turbo compressor, then into the thrust chambers, where
it's mixed with liquid hydrogen and ignited to produce thrust for
the spacecraft.
4. Design Skylon is a fully reusable single stage to orbit
(SSTO) vehicle, able to achieve orbit without staging. The Skylon
spaceplane is designed as a two-engine, "tailless" aircraft, which
is fitted with a steerable canard. The design of the Skylon C2
features a large cylindrical payload bay, 13 m (42 ft. 8 in) long
and 4.8 meters (15 ft. 9 in) in diameter. It is designed to be
comparable with current payload dimensions, and able to support the
containerization of payloads that Reaction Engines hopes for in the
future. The most notable benefit of this would be a dramatic
reduction in the cost of transporting items to orbit. With current
launch vehicles, it costs over $23,000 per kilogram to lift cargo
into orbit.
5. Project Background Skylon is based on a previous project of
Alan Bond, known as HOTOL. The development of HOTOL began in 1982
However, in 1988, the government withdrew further funding, and
development was terminated. The STRICT/STERN designs resulting from
this programme were deemed a great success. According to Management
Today, Skylon has been discussed as a possible replacement for
NASA's Space Shuttle. Skylon could potentially lower satellite
launch costs from the current 15,000/kg to 650/kg.
6. Fuselage and Structure The fuselage of Skylon is expected to
be a carbon fiber space frame; a light and strong structure that
supports the weight of the aluminum fuel tanks and to which the
ceramic skin is attached. Skylon would employ a highly loaded
tightly spaced wheel assembly, to save weight and also interior
space when the wheels are retracted into the fuselage. It will
possess a retractable undercarriage with high pressure tyres and
water-cooled brakes. Skylon will use a low-density fuel, liquid
hydrogen, a great volume is needed to contain enough energy to
reach orbit. Because of the low ballistic coefficient, Skylon would
be slowed at higher altitudes where the air is thinner. As a
result, the skin of the vehicle would only reach 1,100 Kelvin
(K).