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The PW 300 series has been developed in partnership with MTU who are responsible for the low pressure turbine. The first variant, the PW305A, has the following configuration and was designed with a core flexible enough for engines with take-off thrusts from 20 kN to 31 kN (4,500 to 7,000 lb): a single-stage fan driven by a three-stage low pressure turbine, supercharging a four-stage axial ...
The system uses a Terrier first-stage booster attached to an Oriole second-stage rocket. [3] The system can carry payloads between 800 and 1,500 pounds (360 and 680 kg) up to an altitude of 320 kilometres (200 mi). [4] It is also used to test ballistic missile defense systems, under the name ARAV-B.
The SL-3 motor was also test-fired using improvements based on the two previous firings. It resulted in the largest single motor ever fired on Earth at 5.6 million pounds (26.2 meganewtons) of thrust. Since SL-3 used the same casing design and materials as the previous boosters, the change in thrust was obtained from adding a nozzle to the end.
The General Electric YF120, internally designated as GE37, was a variable cycle afterburning turbofan engine designed by General Electric Aircraft Engines in the late 1980s and early 1990s for the United States Air Force's Advanced Tactical Fighter (ATF) program.
The Zenit-2 was the first Zenit to be designed for use as an orbital carrier rocket. It consists of two stages. The first uses an RD-171 engine, and an RD-120 engine powers the second stage.
The Falcon 9 v1.0 first stage was used on the first five Falcon 9 launches, and powered by nine SpaceX Merlin 1C rocket engines arranged in a 3x3 pattern. Each of these engines had a sea-level thrust of 556 kN (125,000 pounds-force) for a total thrust on liftoff of about 5,000 kN (1,100,000 pounds-force).