This change is expected to greatly decrease the granularity of data, improve real-time meteorological information in less traditionally underserved areas, and allowing for smoother real-time weather transitions in-flight. This change will transition the simulator from a current slice-of-time approach using hourly reports to a forward-looking method based on algorithmic predictions. Instead of downloading a large number of METARs local to airports, this version of the simulator will use centrally-processed NOAA GLIB files from a Laminar Research central server which span the globe. The weather system has been overhauled from the ground up. The main landing gear received special attention in that the non-linear strut compression has been modeled to account for the additional downforce which occurs during early takeoff due to the "eagle claw's" rotation. The secondary display page (central bottom display unit) will automatically display the appropriate page for the current phase of flight such as APU start, engine start, cruise, and landing. The Electronic Centralized Aircraft Monitor (ECAM) warning guidance system will recognize failures and provide the crew checklists to remedy the issue. Failure in any primary loop will cause realistic reversion to the backup loop loss of pressure in both primary and secondary loops will cause control system losses. The hydraulic system will simulate all of the components installed in the real aircraft to include the 7 pumps fitted across 3 hydraulic loops - green, blue, yellow. The model features extensive detail to the exterior and a fully-detailed cabin. The aircraft also includes an auto-throttle system complete with the expected thrust modes such as Take-Off/Go-Around (TOGA), Flexible Temperature (FLEX), Maximum Continuous Thrust (MCT), and Maximum Climb Thrust (MCL). Instead adopting a full fly-by-wire architecture, the A330 will respect all of the normal law limitations inherent to Airbus design and intervene to preventing excessing G-loading, overbank, pitch outside of design parameters, and overspeed conditions just as the real aircraft would. It will no longer use crank-and-pulley flight systems which allowed for extreme maneuvers with direct, unfiltered input from the user. Its wingspan is about 15 feet, nd it contains an experiment bay 7 eet long and 4 feet in diameter.Įxperimental demonstrator for Crew Return Vehicle, droppped from a B-52.The Airbus A330 will be the first included heavy aircraft in many years. The X-37 is 27.5eet long - about half the length of the Shuttle payload bay and weighs about 6 tons. Designed to be modular to allow for rapid insertion of technologies and experiments. Remotely piloted research vehicle used to demonstrate the feasibility for a tailless agile fighter.Įxperimental flight vehicle which will integrate and test earth-to-orbit and orbit-to-orbit reusable space transportation technologies. X-35C Joint Advanced Strike Technology (JAST) program full-scale technology demonstrator aircraft intended to validate technologies relevant to fielding a multi-service aircraft with catapult and arresting capability X-35B full-scale technology demonstrator aircraft intended to validate technologies relevant to fielding a multi-service aircraft X-35A first contractor team full-scale technology demonstrator aircraft intended to validate technologies relevant to fielding a multi-service aircraft The vehicle structure is an all-composite with a one piece delta wing design 58 feet in length and 28 feet wide. Goals included speeds up to Mach 8 and altitudes of 250,000 feet, with $500K/flight recurring cost at a rate of 24 flights in 12 months while maintaining a small work force. Reusable technology testbed vehicle to demonstrate technologies for lowering the cost of access to space. X-32C Joint Advanced Strike Technology (JAST) program full-scale technology demonstrator aircraft intended to validate technologies relevant to fielding a multi-service aircraft with catapult and arresting capability X-32B full-scale technology demonstrator aircraft intended to validate technologies relevant to fielding a multi-service aircraft X-32A first contractor team full-scale technology demonstrator aircraft intended to validate technologies relevant to fielding a multi-service aircraft Įnhanced Fighter Maneuverability (EFM) demonstrator with technologies to provide maneuver agility during close-in aerial combat.įirst forward swept wing aircraft toĮxperimental aerospace plane able to operate at hypersonic velocities or accelerating directly into orbit. Piloted orbital flight Provided heat materialsħ configuration. Testbed for Navaho intercontinental cruise missile
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