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CH-53 Super Stallion....
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a few clips stuck together showing a CH-53 Super Stallion airlifting vehicles. |
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My personal test of the Big Super Stallion |
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www.reddogairlines.com
FLIGHT SIMULATOR X RDG CH-53 Super Stallion |
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A collection of pictures and facts highlighing the CH-53 Super Stallion. |
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The world famous annual MCAS Miramar Air Show in San Diego. This CH-53 Super Stallion is a heavy transport unit. As you can see. It can be used to transport a Humvee, or any vehicle up to 16 tons. It can also be used to retrieve downed aircraft. It's loaded with weaponry, such as the M198 howitzers. |
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USMC CH-53 Super Stallion transporting vehicle during Marine Air Ground Task Force (MAGTF) air show demonstration. October 2007 - MCAS Miramar.
Global Defense & Military:
http://www.defencetalk.com/pictures/ |
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a ch-53 "super stallion" helicopter taking off at a helicopter show. |
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FSX CH - 53 Super Stallion Marine Testflight in Grand Canyon Pilot Gentleman |
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Magnifique décollage d'un CH-53 |
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CH-53 in Kandahar Airbase Testflight by Gentleman |
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a ch-53 "super stallion" helicopter flying by at a helicopter show. |
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CH-53E Super Stallion Demonstration
Rotorfest 2001
Brandywine Airport
West Chester, PA
Sunday October 14, 2001
IN THIS VIDEO, watch as this CH-53 performs a demonstration over Brandywine Airport. I apologize in advance for the bad audio tracking, which resulted from a bad conversion to digital quality sound.
If you are interested in purchasing DVDs of specific aircraft or of airshows, interested in everything related to airshows (where the jet teams will be, all airshow performers, airshow reports from airshows I have attended, previews of airshows I will be attending, etc.), and/or everything related to aviation - including spotting guides to my favorite airports and military bases and aircraft factfiles, please check out Steve's Airshow World at www.stevesairshow.com . |
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oh!!! |
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Filmed from another 53 flying in formation |
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Make sure that when you are dropped off by a stallion, you move far away. |
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Air to air footage upload as a test to see if MPEG-4 encoded video in the MPEG-4 Improved format will process and the resulting quality. The aircraft were from Heavy Marine Helicopter Squadron 465 (HMH-465) the Warhorse Squadron. Shot during an aerial refueling exercise. An accident took place during the mission... |
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A thourough tour including facts and pictures of the CH-53 Super Stallion. |
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MH-53E Sea Dragon
Rotorfest 2001
Brandywine Airport
West Chester, PA
Sunday October 14, 2001
IN THIS VIDEO, watch as this MH-53 departs Brandywine Airport and makes one flyby before heading home to Norfolk. I apologize in advance for the bad audio tracking, which resulted from a bad conversion to digital quality sound.
If you are interested in purchasing DVDs of specific aircraft or of airshows, interested in everything related to airshows (where the jet teams will be, all airshow performers, airshow reports from airshows I have attended, previews of airshows I will be attending, etc.), and/or everything related to aviation - including spotting guides to my favorite airports and military bases and aircraft factfiles, please check out Steve's Airshow World at www.stevesairshow.com . |
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Didn't bother to get any closer than this, or else I probably would have ended up on my ass. The ground effect this aircraft has is AMAZING!!!! |
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The CH-53 Sea Stallion is the most common name for the Sikorsky S-65 family of heavy-lift transport helicopters. Originally developed for use by the United States Marine Corps, it is also in service with Germany, Mexico, Iran, Israel, and as the MH-53 Pave Low with the United States Air Force.The USAF also operated the HH-53 "Super Jolly Green Giant" during the late- and post-Viet Nam War era.The dimensionally-similar CH-53E Super Stallion is a heavier-lifting, improved version designated S-80E by Sikorsky. Its third engine makes it more powerful than the Sea Stallion, which it has replaced in the heavy-lift mission.The Sea Stallion has a fuselage design similar to the Sikorsky S-61R/Jolly Green Giant series. It has passenger doors on each side of the fuselage behind the cockpit and a power-operated rear loading ramp. The fuselage was watertight, though not intended for amphibious use, and only landed on water in emergencies. The Stallion has mechanical flight controls which are backed by two independent hydraulic systems. Armor protects crew and vital systems.The CH-53A carries a crew of four; pilot, copilot, crew chief, and "aerial observer", a load of 38 troops, 24 litters with medical attendants, an internal cargo load of 8,000 pounds (3,630 kg) or an external load of 13,000 lb (5,900 kg) on the single-point sling hook. The CH-53A is equipped with a pair of M60 0.308 in (7.62 mm) machine guns that point out to each side of the fuselage.The CH-53A features the six-bladed main rotor and four-bladed tail rotor proven on the S-64. To save space on board naval vessels, the tail boom and the rotors folded. The rotor system was initially driven by twin GE T64-GE-6 turboshafts providing 2,850 shp (2,125 kW) each, with an engine on each side of the forward fuselage. It was later produced with the T64-GE-1 with 3,080 shp (2,300 kW) and then the T64-GE-16 with 3,485 shp (2,600 kW).The HH-53B featured T64-GE-3 engines producing 3,080 shp (2,297 kW).The CH-53D features uprated engines, initially T64-GE-412 with 3,695 shp (2,755 kW) then the T64-GE-413 with 3,925 shp (2,930 kW) with an uprated transmission. Its interior added seats to allow for 55 troops. CH-54Ds are generally armed with twin 0.50 in (12.7 mm) M2/XM218 machine guns.In later years, CH-53Ds have been fitted with defensive countermeasures including an AN/ALQ-39 chaff dispenser and an AN/ALQ-157 infrared set.Later production CH-53Ds featured a Blade Inspection Method (BIM) scheme to detect cracks in its metal rotors. BIM involved pressurizing the interior of the rotor blades. If a crack is present pressure is lost and a red indicator on the rotor blade tip was tripped. Later, the BIM system was connected to a cockpit display. BIM reduced the need to swap out rotor blades on a routine basis.
* Crew: 2 Pilots, 1 or more Crew Chiefs
* Capacity: 37 troops (55 in alternate configuration) or 24 stretchers
* Length: 88 ft 6 in (26.97 m)
* Rotor diameter: 72 ft 2.7 in (22.01 m)
* Height: 24 ft 11 in (7.6 m)
* Empty weight: 23,628 lb (10,740 kg)
* Loaded weight: 33,500 lb (15,227 kg)
* Powerplant: 2× General Electric T64-GE-413 turboshafts, 3,925 shp (2,927 kW) each
* Width (overall): 28 ft 4 in (8.64 m)
* Width (fuselage): 15 ft 6 in (4.7 m)
* Maximum takeoff (Internal Load): 69,750 lb (31,666 kg)
* Maximum takeoff (External Load): 73,500 lb (33,369 kg)
* Maximum speed: 130 kn (241 km/h)
* Range: 540 nmi (1,000 km)
* Service ceiling 16,750 ft (5,106 m)
* Rate of climb: 2,460 ft/min (750 m/min) |
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Big Iron Max Performance Takeoff |
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This video exposes yet again the dangerous, half-assed nature of the USMC egomaniac.
First, the USMC fails to invest in rear ramp fast rope attachment points so two sticks of troops can slide off the rear ramp as one stick goes down the hell hole as the U.S. Army's MH-47E Chinooks have:
http://www.combatreform.com/fries.htm
Thus, exposing the hovering helicopter for MINUTES to enemy fires instead of SECONDS.
Next, the rotor down wash is so severe under the sky-gray (attaboy, USMC) CH-53E Super Stallion heavy lift helicopter, that the fast rope is not even touching the ground! Clearly a WEIGHTED, PADDED, SLIDER carry bag needs to be developed (it could be one of the troops' rucksacks) to pull down on the end of the fast rope to create a ground junction holding the rope vertically so troops don't get injured by not having a clearly visibly point to let go of the rope as depicted in our other FRIES video:
http://www.youtube.com/watch?v=GSdVhuT287w
Reports say the hurricane-downwash V-22 requires WEIGHTED fast ropes so perhaps these will become standard for all VTOL aircraft that use FRIES.
YOUTUBE member drlogic1978 writes:
"I was MIOPS boarding party RN & have done a shitload of fast ropes onto vessels. I agree with the criticisms raised here but would like to point out 1 flaw in US fast roping style. Boots on the rope. Not good. Brits are taught never to put boots on the rope because polish/boot leather streaks the rope making it uber-slippery for the next man down. I personally saw 1 unlucky bitch plummet 20ft on a training tower at HMS Cambridge. Sort this out first USMC! No more gay boot sliding."
While the French Commandos are at least wearing rucksacks simulating mission gear, the gyrenes are not even carrying any M16 assault rifles/M4 carbines! Other videos on YOUTUBE show marines fast roping from the hell hole of smaller CH-46 medium-lift helicopters with rucks and carbines so we know ITS POSSIBLE:
http://www.youtube.com/watch?v=2pqm_SazQKQ
The CH-53E is a great helicopter that was ruined by absurd USMC requirements to carry around a built-in fuselage for foot-slogger victims losing 6 TONS of payload that even early "A" models could have been carrying an Ontos or M113-derived "Mini-Gavin" light tank/APC to gain air-mech capabilities like the Russians do with BMDs and our NATO allies do with Gavins, Scimitars, Bv206es, Vikings, and Wiesels. At the very least, a retracting vehicle floor plate/4-point winch system with extended leg landing gear should be developed to hover insert/extract M113 Mini-Gavins by Streamlined External Loading (SEL) if a place to airland them off the rear ramp is not tactically possible or desirable.
http://www/combatreform.com/nextchinook.htm
If U.S. Army 101st Airborne (Air Assault) troops and gyrenes persist in this dismounted, foot-slogger victim madness
http://www.youtube.com/watch?v=1WDcxfu_v3Q
delivered by slow, loud, vulnerable helicopters not even masked by smokescreens
http://www.combatreform.com/smokescreen.htm
we are going to continue to have debacles like took place daily in Vietnam, the Koh Tang fiasco in 1975, BlackHawk Down! in 1993 and the O'Grady near-disaster in 1995.
http://www.combatreform.com/pathfind.htm
The V-22 can't carry light tracked tanks and should be discarded. The CH-53 should be made into a "Speed Stallion" using Piasecki VTDP/wings technologies so troops in Mini or AmphiGavins
http://www.youtube.com/watch?v=1hbUusptJbs
can be flown in at 250 mph and not get shot-down before getting to fight.
http://www.combatreform.com/piaseckivtdp.htm
Want to know more?
Our book, "Air-Mech-Strike: Asymmetric Maneuver Warfare for the 21st Century" is ONLINE for FREE skyjacked by Google!
http://books.google.com/books?id=RCWtHnYZ0LMC&pg |
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21 APR 2003- Video filmed during aerial refuel of U.S. Marine Corps CH-53E Super Stallion by KC-130 over the South China Sea. Refuel hose and drogue part company from the KC-130, narrowly missing the rotor arc of the CH-53 and spraying aircraft with fuel. Glad I wasn't smoking.. |
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Marine Air Ground Task Force Demonstration
2001 NAS/JRB Willow Grove Air Fest
NAS/JRB Willow Grove, Pennsylvania
Sunday September 9, 2001
IN THIS VIDEO, watch as the MAGTF demonstration takes place at Willow Grove. Participating aircraft include a UH-1N Huey, two AH-1W Cobras, two CH-46 Sea Knights, two CH-53E Super Stallions, a C-130E Hercules, a KC-130R Hercules, two F/A-18 Hornets from VMFA-321, and four A-10s from the 111th Fighter Wing (Pennsylvania ANG).
If you are interested in purchasing DVDs of specific aircraft or of airshows, interested in everything related to airshows (where the jet teams will be, all airshow performers, airshow reports from airshows I have attended, previews of airshows I will be attending, etc.), and/or everything related to aviation - including spotting guides to my favorite airports and military bases and aircraft factfiles, please check out Steve's Airshow World at www.stevesairshow.com . |
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http://www.aviationlive.org Online Aviation Pics,Videos and Forum
The CH-53 Sea Stallion is the most common name for the Sikorsky S-65 family of heavy-lift transport helicopters. Originally developed for use by the United States Marine Corps, it is also in service with Germany, Mexico, Iran, Israel, and as the MH-53 Pave Low with the United States Air Force. The USAF also operated the HH-53 "Super Jolly Green Giant" during the late- and post-Vietnam War era.
The dimensionally-similar CH-53E Super Stallion is a heavier-lifting, improved version designated S-80E by Sikorsky. Its third engine makes it more powerful than the Sea Stallion, which it has replaced in the heavy-lift mission.
In 1960, the US Marine Corps began to seek a replacement for their old S-56 piston-powered helicopters, originally working with the other three U.S. armed services on the "Tri-Service VTOL transport", which would eventually emerge as the Vought-Hiller-Ryan XC-142A tilt-wing. The design became more elaborate and the program stretched out resulting in Marines deciding they couldn't get a workable machine in a satisfactory timeframe and dropped out. This was just as well, because the XC-142A, although a very innovative and capable machine, would never enter production.
In March 1962, the US Navy Bureau of Weapons, acting on behalf of the Marines, issued a request for a "Heavy Helicopter Experimental / HH(X)". The specifications dictated a load capability of 8,000 pounds (3,630 kilograms) with an operational radius of 100 NM (185 km) at a speed of 150 kt (278 km/h). The HH(X) was to be used in the assault transport, aircraft recovery, personnel transport, and medical evacuation roles. In the assault transport role, it was to be mostly used to haul heavy equipment instead of troops.
In response, Boeing Vertol offered a modified version of the Chinook; Kaman offered a development of the British Fairey Rotodyne compound helicopter; and Sikorsky offered what amounted to a scaled-up version of the S-61R, with twin GE T64 turboshafts and the dynamic system of the S-64, to be designated the "S-65". Kaman's proposal quickly died when the British government dropped its backing of the Rotodyne program. Competition between Boeing Vertol and Sikorsky was intense, with the Boeing Vertol having something of an edge because the type was being acquired by the U.S. Army. Sikorsky threw everything into the contest and was awarded the contract in July 1962.
HMH-362 CH-53Ds landing.
HMH-362 CH-53Ds landing.
The Marines originally wanted to buy four prototypes but ran into funding problems. Sikorsky, determined to keep the deal, cut their estimate for development costs and said that the program could be done with two prototypes. The military bought off on the proposal, and in September 1962 Sikorsky was awarded a contract for a little under US$10 million for two "YCH-53A" prototypes, as well as a mockup and a ground-test airframe.
The development program did not go entirely smoothly, due to a shortage of engineering resources plus various failures of subcontractors and the government, but these problems were gradually overcome. There was also the problem that U.S. Defense Secretary Robert S. McNamara was pushing "commonality" between the armed services and pressuring the Marines to obtain the Chinook anyway, but the Marines managed to convince McNamara's people that the Chinook couldn't meet requirements without a lot of expensive changes.
All these obstacles overcome, the first YCH-53A performed its initial flight at the Sikorsky plant in Stratford, Connecticut, on October 14, 1964, about four months behind schedule. The Marines had already placed an initial production contract for 16 helicopters in September. Flight trials went more smoothly than expected, helping make up for the lost time in development. It received the military designation and name "CH-53A Sea Stallion". Delivery of production CH-53s began in 1966. |
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With the Lack of a Mule an Air Show worker volunteered his truck to tow this HUGE Helicopter during Rotor Fest 2006 at Brandywine Airport in West Chester, PA. New Comercial for Dodge? |
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Us Army preparing in the event that bad forces try to invade one of are Schools hear in the USA.... Pave low MH-60R Sea hawk MH-60S Knight hawk HH-60 Jay hawk .... |
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