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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.
Launch operations are supervised and controlled from several control rooms known as firing rooms. The controllers are in control of pre-launch checks, the booster and spacecraft. Once the rocket has cleared the launch tower (usually within the first 10–15 seconds), is when control is switched over to the mission's relative mission control center.
The missile launch control environment also varied by system. Early missiles such as Thor and Atlas, relied on support facilities above ground, with crews protected in a shelter of some sort. Later systems were buried underground, either with the missiles located nearby (i.e. Titan) or a distance away (Peacekeeper, Minuteman).
Before significant events, the flight director will "go around the room", polling each controller for a go/no go decision, a procedure also known as a launch status check. If all factors are good, each controller calls for a "go" but if there is a problem requiring a hold or an abort, the call is "no go".
The ALE-50 system consists of a launcher and launch controller installed on the aircraft (usually on a wing pylon), and one or more expendable towed decoys. Each decoy is delivered in a sealed canister and has a ten-year shelf life. [2]
The first rule set was simply known as AeroTech and later referred to as AeroTech 1 or AT1. The AT1 release was a large introduction box set that could be played as a complete independent game that co-exists in the BattleTech universe, compatible with the regular ground game. The rule set introduced aerospace fighters (space/air-capable fighter ...
For Space Shuttle missions, in the firing room at the Launch Control Center, the NASA Test Director (NTD) performed this check via a voice communications link with other NASA personnel. The NTD was the leader of the shuttle test team responsible for directing and integrating all flight crew, orbiter, external tank/solid rocket booster and ...
Reaction control systems are capable of providing small amounts of thrust in any desired direction or combination of directions. An RCS is also capable of providing torque to allow control of rotation (roll, pitch, and yaw). [2] Reaction control systems often use combinations of large and small thrusters, to allow different levels of response.
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