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Fuerzas Terrestres
Noticias y Actualidad de las Fuerzas Terrestres
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<blockquote data-quote="Daniel1962" data-source="post: 2313811" data-attributes="member: 4365"><p>Los CH-53 que citaron fueron los modelo K, actualmente en producción.</p><p></p><p><span style="font-size: 18px"><strong> (CH-53K)</strong></span></p><p>* = data for K model. All others for E model.</p><p></p><p><em>Data from</em> Sikorsky CH-53K sources,<a href="https://en.wikipedia.org/wiki/Sikorsky_CH-53K_King_Stallion#cite_note-CH-53K_broch-48">[48]</a><a href="https://en.wikipedia.org/wiki/Sikorsky_CH-53K_King_Stallion#cite_note-CH-53K_attributes-57">[57]</a><a href="https://en.wikipedia.org/wiki/Sikorsky_CH-53K_King_Stallion#cite_note-CH-53K_brief-60">[60]</a> GE38-1B data,<a href="https://en.wikipedia.org/wiki/Sikorsky_CH-53K_King_Stallion#cite_note-GE_GE38-1B-47">[47]</a> Flightglobal.com<a href="https://en.wikipedia.org/wiki/Sikorsky_CH-53K_King_Stallion#cite_note-Flightglobal.com-61">[61]</a></p><p></p><p><strong>General characteristics</strong></p><p></p><ul> <li data-xf-list-type="ul"><strong>Crew:</strong> 5: 2 pilots, 1 crew chief/right gunner, 1 left gunner, 1 tail gunner (combat crew)</li> <li data-xf-list-type="ul"><strong>Capacity:</strong> 37 troops (55 with centerline seats installed)</li> <li data-xf-list-type="ul"><strong><a href="https://en.wikipedia.org/wiki/Payload">Payload</a>:</strong> * 35,000 lb (15,900 kg)</li> <li data-xf-list-type="ul"><strong>Length:</strong> 99 ft 1/2 in (30.2 m)</li> <li data-xf-list-type="ul"><strong>Rotor diameter:</strong> 79 ft (24 m)</li> <li data-xf-list-type="ul"><strong>Height:</strong> 27 ft 9 in (8.46 m)</li> <li data-xf-list-type="ul"><strong>Disc area:</strong> 4,900 ft² (460 m²)</li> <li data-xf-list-type="ul"><strong><a href="https://en.wikipedia.org/wiki/Manufacturer%27s_empty_weight">Empty weight</a>:</strong> 33,226 lb (15,071 kg)</li> <li data-xf-list-type="ul"><strong>Loaded weight:</strong> 74,000 lb (33,600 kg)</li> <li data-xf-list-type="ul"><strong><a href="https://en.wikipedia.org/wiki/Maximum_takeoff_weight">Max. takeoff weight</a>:</strong> * 84,700 lb (38,400 kg)</li> <li data-xf-list-type="ul"><strong>Rotor systems:</strong> 7 blades on main rotor (each 35' × 35"), 4 blades on tail rotor</li> <li data-xf-list-type="ul"><strong><a href="https://en.wikipedia.org/wiki/Aircraft_engine">Powerplant</a>:<span style="font-size: 22px"> 3 </span></strong>× *<a href="https://en.wikipedia.org/wiki/GE-Aviation">General Electric</a> <a href="https://en.wikipedia.org/wiki/General_Electric_GE38">GE38-1B</a> <a href="https://en.wikipedia.org/wiki/Turboshaft">turboshaft</a>, * 7,500 shp (5,600 kW) each</li> </ul></blockquote><p></p>
[QUOTE="Daniel1962, post: 2313811, member: 4365"] Los CH-53 que citaron fueron los modelo K, actualmente en producción. [SIZE=5][B] (CH-53K)[/B][/SIZE] * = data for K model. All others for E model. [I]Data from[/I] Sikorsky CH-53K sources,[URL='https://en.wikipedia.org/wiki/Sikorsky_CH-53K_King_Stallion#cite_note-CH-53K_broch-48'][48][/URL][URL='https://en.wikipedia.org/wiki/Sikorsky_CH-53K_King_Stallion#cite_note-CH-53K_attributes-57'][57][/URL][URL='https://en.wikipedia.org/wiki/Sikorsky_CH-53K_King_Stallion#cite_note-CH-53K_brief-60'][60][/URL] GE38-1B data,[URL='https://en.wikipedia.org/wiki/Sikorsky_CH-53K_King_Stallion#cite_note-GE_GE38-1B-47'][47][/URL] Flightglobal.com[URL='https://en.wikipedia.org/wiki/Sikorsky_CH-53K_King_Stallion#cite_note-Flightglobal.com-61'][61][/URL] [B]General characteristics[/B] [LIST] [*][B]Crew:[/B] 5: 2 pilots, 1 crew chief/right gunner, 1 left gunner, 1 tail gunner (combat crew) [*][B]Capacity:[/B] 37 troops (55 with centerline seats installed) [*][B][URL='https://en.wikipedia.org/wiki/Payload']Payload[/URL]:[/B] * 35,000 lb (15,900 kg) [*][B]Length:[/B] 99 ft 1/2 in (30.2 m) [*][B]Rotor diameter:[/B] 79 ft (24 m) [*][B]Height:[/B] 27 ft 9 in (8.46 m) [*][B]Disc area:[/B] 4,900 ft² (460 m²) [*][B][URL='https://en.wikipedia.org/wiki/Manufacturer%27s_empty_weight']Empty weight[/URL]:[/B] 33,226 lb (15,071 kg) [*][B]Loaded weight:[/B] 74,000 lb (33,600 kg) [*][B][URL='https://en.wikipedia.org/wiki/Maximum_takeoff_weight']Max. takeoff weight[/URL]:[/B] * 84,700 lb (38,400 kg) [*][B]Rotor systems:[/B] 7 blades on main rotor (each 35' × 35"), 4 blades on tail rotor [*][B][URL='https://en.wikipedia.org/wiki/Aircraft_engine']Powerplant[/URL]:[SIZE=6] 3 [/SIZE][/B]× *[URL='https://en.wikipedia.org/wiki/GE-Aviation']General Electric[/URL] [URL='https://en.wikipedia.org/wiki/General_Electric_GE38']GE38-1B[/URL] [URL='https://en.wikipedia.org/wiki/Turboshaft']turboshaft[/URL], * 7,500 shp (5,600 kW) each [/LIST] [/QUOTE]
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