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CUVX Design Report - the AOE home page - Virginia Tech

CUVX Design Report - the AOE home page - Virginia Tech

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<strong>CUVX</strong> <strong>Design</strong> – VT Team 2 Page 704.6.3 EMALSTwo Electro-Magnetic Aircraft Launching Systems (EMALS) are used for launching aircraft. The launch deckis fully automated and unmanned. Both <strong>the</strong> UCAVs and UAVs are launched using EMALS. This new technologyreplaces <strong>the</strong> standard steam driven catapults currently in use on CVNs. <strong>CUVX</strong>-HI3 has two EMALS positionedside-by-side and staggered on <strong>the</strong> launch deck. The EMALS are 75 meters (starboard) and 85 meters (port) long, 3meters deep, 1 meter wide, and weighs approximately 220 MT. The 75 meter length is sufficient for <strong>the</strong> take-offrequirements of VT UCAV-N and Shadow 400. The aircraft shuttle starts 1.5 meters from <strong>the</strong> beginning of <strong>the</strong>track. It is estimated that 30 MW of power will be required to launch a single UCAV and <strong>the</strong> cycle time betweensuccessive launches is around 45 seconds depending on <strong>the</strong> amount of cooling. The tracks are spaced at a 2 degreeangle about <strong>the</strong> centerline and taper to 1.5 meters apart at <strong>the</strong> end. The machinery required for <strong>the</strong> system is locatedunderneath <strong>the</strong> launch deck in <strong>the</strong> area above <strong>the</strong> pilot house. The control systems for EMALS are accessible from<strong>the</strong> pilot house, but located in a low profile enclosed control center situated on <strong>the</strong> port side of <strong>the</strong> launch deck. Thisallows <strong>the</strong> flight control operator to view launch operations while protected by an enclosed environment. OneEMALS will be used as <strong>the</strong> primary launcher; <strong>the</strong> second system is available for redundancy. Figure 62 showscritical dimensions of <strong>the</strong> EMALS on <strong>the</strong> launch deck. Refer to Section 3.2.5.3 for additional information.Figure 62. Dimensioned Launch Deck and EMALS4.6.4 Jet Blast DeflectorsThere is a jet blast deflector/door 10 meters aft of <strong>the</strong> launch ramp on <strong>the</strong> ship’s launch deck that separates <strong>the</strong>launch deck from Hangar Deck 1. The port side of <strong>the</strong> deflector is a movable door that slides behind <strong>the</strong> starboardside of <strong>the</strong> deflector to allow aircraft through from Hangar Deck 1 out onto <strong>the</strong> launch deck. Both sides of <strong>the</strong>deflector are angled down and aft from <strong>the</strong> centerline to direct <strong>the</strong> exhaust from launch out <strong>the</strong> vented sides of <strong>the</strong>ship. The doors remain closed when <strong>the</strong>re are no aircraft operations taking place, and must be closed before planescan be launched. The deflector has chilled water piped through it to dissipate <strong>the</strong> jet exhaust heat. It is estimatedthat this deflector will weigh 30 MT and will require 100 kW of power to open and close during aircraft launchoperations. A rendering of <strong>the</strong> jet blast deflector is shown in Figure 63. Refer to Figure 62 for its location on <strong>the</strong>launch deck.4.6.5 Arresting Gear and Recovery DeckFigure 63. Jet Blast DeflectorCable arresting gear is used to recover aircraft on <strong>the</strong> recovery deck. There are three cables in this system for<strong>the</strong> aircraft to catch, evenly spaced seven meters apart. The first arresting cable is 15 meters from <strong>the</strong> aft deck edge.Limitations in <strong>the</strong> length of <strong>the</strong> recovery deck limit <strong>the</strong> spacing between <strong>the</strong>se cables to be closer than on CVN.However, <strong>the</strong> spacing is sufficient for <strong>the</strong> landing of precision computer-controlled aircraft with <strong>the</strong> lower landing

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