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  2. Launch vehicle system tests - Wikipedia

    en.wikipedia.org/wiki/Launch_vehicle_system_tests

    After 55 seconds of flight, a command was sent to cut propulsion, and the rocket crashed 4 miles (6 km) or 5 miles (8 km) downrange. [12]: 172–181 On June 30th, 2024, during a static fire test of the first stage of the Space Pioneer Tianlong-3, a structural failure between the rocket and test stand resulted in an unintentional launch.

  3. Launch Vehicle Digital Computer - Wikipedia

    en.wikipedia.org/wiki/Launch_Vehicle_Digital...

    LVDC from Instrument Unit technical manual. The Launch Vehicle Digital Computer (LVDC) was a computer that provided the autopilot for the Saturn V rocket from launch, through Earth orbit insertion, and the trans-lunar injection burn that would send the Apollo spacecraft to the Moon.

  4. Integrated Powerhead Demonstrator - Wikipedia

    en.wikipedia.org/wiki/Integrated_powerhead...

    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 ...

  5. Warner Bros. Releases 31 Full-Length Movies on Its YouTube ...

    www.aol.com/warner-bros-releases-31-full...

    Here’s the full list of titles from Warner Bros. currently available for free on YouTube: “The Wind and the Lion” (1975) starring Sean Connery “Michael Collins” (1996)

  6. LauncherOne - Wikipedia

    en.wikipedia.org/wiki/LauncherOne

    The rocket had a diameter of 1.6 m (5 ft 3 in) for the first stage and 1.3 m (4 ft 3 in) for the second stage and payload fairing. [ 4 ] On the 24th of October 2019, the company announced plans to develop a three-stage variant that would be capable of launching 100 kg (220 lb) to the Moon , 70 kg (150 lb) to Venus , or 50 kg (110 lb) to Mars .

  7. Athena (rocket family) - Wikipedia

    en.wikipedia.org/wiki/Athena_(rocket_family)

    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).

  8. Aerospike engine - Wikipedia

    en.wikipedia.org/wiki/Aerospike_engine

    The rocket is designed to send up to 100 kg into low-Earth orbit, at a price of US$1 million per launch. [9] They later announced that their Executor Aerospike engine would produce 50,500 pounds-force (225 kN) of thrust at sea level and 73,800 pounds-force (328 kN) of thrust in a vacuum.

  9. Space Launch System core stage - Wikipedia

    en.wikipedia.org/wiki/Space_Launch_System_core_stage

    The Space Launch System core stage, or simply core stage, is the main stage of the American Space Launch System (SLS) rocket, built by The Boeing Company in the NASA Michoud Assembly Facility. At 65 m (212 ft) tall and 8.4 m (27.6 ft) in diameter, the core stage contains approximately 987 t (2,177,000 lb) of its liquid hydrogen and liquid ...