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On July 19, 2006 Rocketdyne announced that the demonstrator engine front-end had been operated at full capacity. [3]According to NASA, the Integrated Powerhead Demonstrator project was the first of three potential phases of the Integrated High Payoff Rocket Propulsion Technology Program, which was aimed at demonstrating technologies that double the capability of state-of-the-art cryogenic ...
The K239 Chunmoo is a self-propelled multiple launch rocket system (MLRS) capable of firing several different guided or unguided artillery rockets. The K239 is capable of launching K33 131 mm rockets, but not 130 mm rockets (such as the K30, K37 and K38), which are used in the existing K136 Kooryong rocket artillery system.
The designation was later reused for a proposed rocket for the Commercial Orbital Transportation Services project. Sometime after 2005, PlanetSpace reused the Athena III designation for a 2.8-million-pound-thrust shuttle-derived space station resupply booster rocket, in a joint venture with Lockheed Martin and Alliant Techsystems (ATK).
NASA started full-engine, hot-fire testing in March, 1999, with a 20 second test to demonstrate the complete engine system. [12] The engine was tested at full power for 155 seconds on July 1, 1999. [13] A total of 85 tests were scheduled for the rest of 1999. As of 2000, 48 tests had been conducted on three engines using three test stands. [8]
The Nike Tomahawk has a Nike rocket as the first stage, and a Tomahawk rocket as the second. The Nike Tomahawk has a ceiling of 230 statute miles (370 km), a payload capacity of 100 pounds (45 kg), a launch thrust of 49,000 pounds of force (217 kN ), a launch weight of 2,200 pounds (1,000 kg), a diameter of 17 inches (0.43 m) and a length of 35 ...
The Zenit first stage was used as a strap-on booster rocket for the Energia carrier rocket. [12] Four Zenit first stages were attached to the core vehicle to produce extra thrust at lift-off, in the same way that Solid Rocket Boosters were used on the US Space Shuttle. Energia made two flights (1987 and 1988) before the programme was abandoned.
The processor and software direct data to and from the instruments, to the solid-state memory core, and to the radio system which can send data back to Earth and receive commands. [10] The computer also controls the pointing and movement of the spacecraft, taking in sensor data from the gyroscopes and star tracker , and sending the necessary ...
The original version of the SURA rocket, the SURA 80R, was developed by Hispano-Suiza in the 1960s. [1] In 1971 Oerlikon-Buhrle took over the military division of Hispano-Suiza and redesignated the SURA 80R, the SURA-FL, and further developed the SURA-FL which is the current SURA-D. [ note 1 ] The SNORA rockets can be fired from either a ...
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