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A development version of Orion's crew module was launched in 2014 during Exploration Flight Test-1, while at least four test articles were produced. Orion was primarily designed by Lockheed Martin Space Systems in Littleton, Colorado, with former Space Shuttle engineer Julie Kramer White at NASA as Orion's chief engineer. [6]
Orion's design consists of three main parts: a crew module (CM) similar to the Apollo command module, but capable of sustaining four to six crew members; a cylindrical service module (SM) containing the primary propulsion systems and consumable supplies; and the Launch Abort System (LAS), which provides capability for the astronauts and Crew ...
Orion, as a later design, after the initial plans for the Crew Exploration Vehicle led to development of the Orion. The Crew Exploration Vehicle (CEV) was a component of the U.S. NASA Vision for Space Exploration plan. A competition was held to design a spacecraft that could carry humans to the destinations envisioned by the plan.
At the top of the Ares I-X flight test vehicle was a combined Orion crew module and launch abort system simulator, resembling the structural and aerodynamic characteristics of Ares I. The full-scale crew module (CM) is approximately 16 feet (4.9 m) in diameter and 7 feet (2.1 m) tall, while the launch abort system (LAS) is 46 feet (14 m) long.
Artist's rendition of the docking of Orion to the ISS Ares I-X launches from LC-39B, 15:30 UTC, October 28, 2009.. The Constellation Program was NASA's planned future human spaceflight program between 2005 and 2009, which aimed to develop a new crewed spacecraft and a pair of launchers (Ares I and Ares V) to continue servicing the International Space Station and return to the Moon.
A close-up of a government-reference airlock module for the Gateway Space Station. Mission planning calls for an airlock to be delivered and integrated to Gateway by the crewed Orion spacecraft on the Artemis VI mission after launching on an Space Launch System (SLS) Block 1B rocket.
A launch escape system (LES) or launch abort system (LAS) is a crew-safety system connected to a space capsule. It is used in the event of a critical emergency to quickly separate the capsule from its launch vehicle in case of an emergency requiring the abort of the launch, such as an impending explosion.
Navy divers assist NASA to recover a mock-up of NASA's Orion crew module that will splash down in the Pacific Ocean concluding the Artemis I mission.