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  2. SpaceX Crew-8 - Wikipedia

    en.wikipedia.org/wiki/SpaceX_Crew-8

    Crew-8 was the eighth SpaceX operational mission in the Commercial Crew Program and the 13th overall crewed orbital flight of a Crew Dragon spacecraft. [8] The mission launched at 3:53:38 UTC on 4 March 2024 (3 March, 10:53:38 pm EST, local time at the launch site). [9] SpaceX sent the 50th astronaut on this Crew Dragon launch. [10]

  3. Commercial Crew Program - Wikipedia

    en.wikipedia.org/wiki/Commercial_Crew_Program

    SpaceX Crew-2 launched on 23 April 2021 and it landed on 9 November 2021, two days before the launch of SpaceX Crew-3. When Boeing OFT-2 was on the pad preparing for launch on 3 August 2021, problems were encountered with 13 valves in the capsule's propulsion system. The launch was scrubbed, and the capsule eventually returned to the factory.

  4. Crew Dragon Launch Abort System - Wikipedia

    en.wikipedia.org/.../Crew_Dragon_Launch_Abort_System

    A figure showing the Apollo spacecraft's launch abort system. A diagram showing the configuration of Crew Dragon Endeavor during the Demo-2 mission.. Traditionally, spacecraft like Apollo and Soyuz have utilized solid-fueled "puller" launch escape systems, with the main spacecraft beneath a protective fairing attached to the escape system.

  5. Crew Dragon Endeavour - Wikipedia

    en.wikipedia.org/wiki/Crew_Dragon_Endeavour

    Crew-8: 4 March 2024, 3:53:38 25 October 2024, 07:29:02 235 days, 3 hours, 35 minutes Longest Crew Dragon mission to date. Ferried four Expedition 70/71/72 crew members to the ISS. ISS stay extended and two makeshift seats added to allow spacecraft to serve as "lifeboat" for Boeing CFT crew if needed. [32]

  6. Apollo 8 - Wikipedia

    en.wikipedia.org/wiki/Apollo_8

    Apollo 8 was planned as the "D" mission, a test of the LM in a low Earth orbit in December 1968 by James McDivitt, David Scott, and Russell Schweickart, while Borman's crew would fly the "E" mission, a more rigorous LM test in an elliptical medium Earth orbit as Apollo 9, in early 1969. The "F" Mission would test the CSM and LM in lunar orbit ...

  7. Orion (spacecraft) - Wikipedia

    en.wikipedia.org/wiki/Orion_(spacecraft)

    [13] [14] [15] The crew module is the only part of the spacecraft that returns to Earth after each mission and is a 57.5° frustum shape with a blunt spherical aft end, 5.02 meters (16 ft 6 in) in diameter and 3.3 meters (10 ft 10 in) in length, [16] with a mass of about 8.5 metric tons (19,000 lb).

  8. Comparison of crewed space vehicles - Wikipedia

    en.wikipedia.org/wiki/Comparison_of_crewed_space...

    Launch system Crew size Length (m) Diameter (m) Launch mass (kg) Power system Generated power (W) Recovery method First spaceflight § Last spaceflight Flights § SpaceShipOne USA: Scaled Composites: 112 km X Prize: White Knight Hybrid Motor: 1: 8.53 8.05 3,600 Batteries Runway landing 2004: 2004: 3 [note 22] X-15 USA: North American Aviation ...

  9. SpaceX Crew-1 - Wikipedia

    en.wikipedia.org/wiki/SpaceX_Crew-1

    SpaceX Crew-1 [6] [7] (was also known as USCV-1 or simply Crew-1) [8] was the first operational [b] crewed flight of a Crew Dragon spacecraft, and the maiden flight of the Crew Dragon Resilience spacecraft. It was also the second crewed orbital flight launch by the United States since that of STS-135 in July 2011.