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Post by elangguntur on Sept 5, 2008 7:27:20 GMT 7
Nggak banyak populasinya didunia, hanya Russia dan Amerika yang mengembangkannya, panjangnya rata2 lebih dari 30 Meter.
AURI (TNI-AU) sempat mengopeasikan heli ini, Mi-6 Hook. Kalau pingin dapet kisahnya lengkap, silahkan cari buku SEGESIT PUMA SEKUAT GAJAH tulisan Sugiyono tentang skadron 8.
Berikut Heli2 tersebut, Russia : Mi-6 Hook Role Heavy transport helicopter Manufacturer Mil Moscow Helicopter Plant First flight 5 September 1957[1] Introduction 1962 Retired 2002 (Russia CAA) Status In service with foreign users Primary users Soviet Air Force Aeroflot Produced 1960 to 1981[2] Number built 925+ Variants Mil Mi-10 Mil Mi-26
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Post by elangguntur on Sept 5, 2008 7:37:01 GMT 7
Russia : Mi-6 Hook Role: Heavy transport helicopter Manufacturer: Mil Moscow Helicopter Plant First flight: 5 September 1957[1] Introduction: 1962 Retired 2002: (Russia CAA) Status In service: with foreign users Primary users: Soviet Air Force, Aeroflot Produced: 1960 to 1981[2] Number built: 925+ Variants: Mil Mi-10, Mil Mi-26 General characteristics Crew: Five Capacity: 61 troops or up to 12,000 kg (26,400 lb) of cargo Length: 33.18 m (108 ft 10 in) Rotor diameter: 35.00 m (114 ft 10 in) Height: 9.86 m (32 ft 4 in) Disc area: 962 m² (10,350 ft²) Empty weight: 26,500 kg (58,400 lb) Loaded weight: 39,700 kg (87,500 lb) Max takeoff weight: 41,700 kg (91,900 lb) Powerplant: 2× Soloviev D-25V turboshafts, 4,100 kW (5,500 shp each) each Performance Maximum speed: 300 km/h (188 mph) Range: 500 km (310 miles) Service ceiling 4,500 m (14,800 ft) Disc loading: 41 kg/m² (8 lb/ft²) Power/mass: 0.21 kW/kg (0.13 hp/lb) negara operator
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Post by elangguntur on Sept 5, 2008 7:41:57 GMT 7
Mil Mi-12: Role: Heavy lift helicopter Manufacturer : Mil Design Bureau First flight : 10 July 1968 Status : Prototype only Primary user : Soviet Union Number built : only 2 Developed from Mil Mi-6 General characteristics Crew: Six Capacity: Up to 40,000 kg (88,000 lb) of cargo Length: 37.00 m (121 ft 4 in) Rotor diameter: 2x 35.00 m (114 ft 10 in) Height: 12.50 m (41 ft 0 in) Disc area: 1,924 m² (20,700 ft²) Empty weight: 69,100 kg (152,000 lb) Loaded weight: 97,000 kg (213,400 lb) Max takeoff weight: 105,000 kg (231,000 lb) Powerplant: 4× Soloviev D-25VF turboshafts, 4,048 kW (6,497 shp) each Performance Maximum speed: 260 km/h (163 mph) Range: 1,000 km (625 miles) Service ceiling 3,500 m (11,480 ft) Disc loading: 50 kg/m² (10 lb/ft²) Power/mass: 0.20 kW/kg (0.12 hp/lb)
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Post by elangguntur on Sept 5, 2008 8:09:51 GMT 7
Mi-26: Role: Heavy Lift Helicopter National origin : Soviet Union - Russia Manufacturer: Mil Moscow Helicopter Plant First flight : 14 December 1977 Introduction : 1983 Status : Active Primary users : Russian Air Force, Aeroflot Produced : 1981 to present Number built : 200 Developed from Mil Mi-6 General characteristics Crew: Six – 2 pilots, 1 navigator, 1 flight engineer, 1 loadmaster, 1 radio/electronic systems operator Capacity: Up to 150 troops, 90 recommended 20,000 kg cargo (44,000 lbs) Length: 40.025 m (131 ft 4 in) (rotors turning) Rotor diameter: 32.00 m (104 ft 11.8 in) Height: 8.145 m (26 ft 9 in) Disc area: 789m² (8,495 ft²) Empty weight: 28,200 kg (62,170 lb) Loaded weight: 49500 kg (108,900 lb) Max takeoff weight: 56,000 kg (123,500 lb) Powerplant: 2× Lotarev D-136 turboshafts, 8,380 kW (11,240 shp) each Performance Maximum speed: 295 km/h, 183 mph (160 kt) Range: 1,952 km, 1,240 miles (1,080 nautical miles) Service ceiling 4,600 m (15,100 ft)
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Post by elangguntur on Sept 9, 2008 12:47:51 GMT 7
Lanjut ke amerika dari Sikorsky: CH-53E Super Stallion Role : Heavy-lift cargo helicopter Manufacturer : Sikorsky Aircraft Introduced : 1981 Status : Active service Primary users : United States Marine Corps, United States Navy, Japan Maritime-SDF Number built : 115 Unit cost : US$24.36 million (1992) average[1] Developed from CH-53 Sea Stallion General characteristics Crew: 5: 2 pilots, 1 crew chief/right gunner, 1 left gunner, 1 tail gunner (combat crew) Capacity: 37 troops (55 with centerline seats installed) Payload: 32,000 lb (15,000 kg) Length: 99 ft 1/2 in (30.2 m) Rotor diameter: 79 ft (24 m) Height: 27 ft 9 in (8.46 m) Disc area: 4,900 ft² (460 m²) Empty weight: 33,226 lb (15,071 kg) Max takeoff weight: 73,500 lb (33,300 kg) Powerplant: 3× General Electric T64-GE-416(A) turboshafts, 4,380 shp (3,270 kW) each Rotor systems: 7 blades on main rotor Performance Maximum speed: 170 knots (196 mph, 315 km/h) Cruise speed: 150 kt (173 mph, 278 km/h) Range: 540 nmi (621 mi, 1,000 km) Ferry range: 990 nmi (1,139 mi, 1,833 km) Service ceiling 18,500 ft (5,640 m) Rate of climb: 2,500 ft/min (13 m/s) Armament Guns: 2× .50 BMG (12.7 x 99 mm) window-mounted XM218 machine guns 1× .50 BMG (12.7 x 99 mm) ramp mounted weapons system, GAU-21 (M3M mounted machine gun) Other: Chaff and flare dispensers
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Post by elangguntur on Sept 9, 2008 12:56:33 GMT 7
HH-53 "Super Jolly Green Giant" / MH-53 Pave Low Pengembangan dari Heli Sikorsky CH-53 Sea Stallion untuk program : helicopter for long-range combat search and rescue (CSAR) untuk menggantikan HH-3 "Jolly Green Giant", Heli ini kemudian di-upgrad lagi dan dikenal sebagai MH-53 Pave Low. Role Heavy-lift helicopter Manufacturer : Sikorsky Aircraft Status : Active Primary user : United States Air Force Unit cost MH-53J: US$40 million (2001 dollars) Developed from CH-53 Sea Stallion General characteristics Crew: 6 (two pilots, two flight engineers and two gunners) Capacity: approx. 38 troops Length: 88 ft (28 m) Rotor diameter: 72 ft (21.9 m) Height: 25 ft (7.6 m) Empty weight: 32,000 lb (14,515 kg) Max takeoff weight: 46,000 lb (50,000 lb in war time) (21,000 kg) Powerplant: 2× T64-GE-100 turboshafts, 4,330 shp (3,230 kW) each Rotor system: 6 blades Performance Maximum speed: 170 knots (196 mph, 315 km/h) Cruise speed: 150 kt (173 mph, 278 km/h) Range: 600 NM (1,100 km) Service ceiling 16,000 ft (4,900 m) Armament Any combination of three 7.62 mm mini guns or .50 caliber (12.7 mm) machine guns mounted on left and right sides (immediately behind flight deck) and ramp.
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Post by elangguntur on Sept 9, 2008 13:05:46 GMT 7
Andalan Boeing yang cukup laku, di operasikan lebih di 20 negara di dunia. Kabarnya TNI-AU sempet tertarik dengan heli ini setelah melihat performanya saat penanggulangan Tsunami Aceh lalu. Terdapat banyak variant: Variants 1 CH-47A 2 ACH-47A 3 CH-47B 4 CH-47C 5 CH-47D 6 MH-47D 7 MH-47E 8 CH-47F 9 MH-47G 10 HH-47 11. export models 12 Civilian models CH-47 Chinook Role : Cargo helicopter Manufacturer : Boeing Helicopters First flight : 21 September 1961 Introduction : 1962 Status : Active service Primary users : United States Army, Australian Army, Japan-GSDF, Force, Royal Netherlands-AF Number built more than 1,179[1] Unit cost $10.3 million (1999)[2] Developed from CH-46 Sea Knight General characteristics Crew: 3 (pilot, copilot, flight engineer) Capacity: 33-55 troops or 24 litters and 3 attendants 28,000 lb (12,700 kg) cargo Length: 98 ft 10 in (30.1 m) Rotor diameter: 60 ft 0 in (18.3 m) Height: 18 ft 11 in (5.7 m) Disc area: 2,800 ft² (260 m²) Empty weight: 23,400 lb (10,185 kg) Loaded weight: 26,680 lb (12,100 kg) Max takeoff weight: 50,000 lb (22,680 kg) Powerplant: 2× Lycoming T55-GA-712 turboshafts, 3,750 hp (2,796 kW) each Performance Maximum speed: 170 knots (196 mph, 315 km/h) Cruise speed: 130 kt (137 mph, 220 km/h) Range: 400 nmi (450 mi, 741 km) Service ceiling 18,500 ft (5,640 m) Rate of climb: 1,522 ft/min (10.1 m/s) Disc loading: 9.5 lb/ft² (47 kg/m²) Power/mass: 0.28 hp/lb (460 W/kg) Armament M134 7.62 mm (0.308 in) minigun, M240 7.62 mm (0.308 in) machine gun Avionics Rockwell CAAS (MH-47G/CH-47F)
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Post by cakrabyuha on Sept 9, 2008 22:34:02 GMT 7
Kalo boleh milih, saya pilih Mi-26 aja deh bisa gotong Chinook, ama gak rawan Embargo...
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Post by elangguntur on Sept 10, 2008 14:46:50 GMT 7
setuju pisan, dulu kita juga pernah punya 9 buah Mi-6. Sekarang kalo bisa 12 atau 16 lah cukup.
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Post by elangguntur on Sept 16, 2008 11:48:40 GMT 7
Heli raksasa lainnya: Mil Mi-10 Dikembangkan dari Heli Mi-6 sebagai heavy flying crane. Tampil perdana di depan publik pada tahun 1961. Technical data for Mi-10 Engine: 2 x D-25V turboshaft, rated at 4045kW, main rotor diameter: 35.0m, length without rotors: 32.86m, height: 7.8m, take-off weight: 43450kg, empty weight: 24680kg, max speed: 235km/h, cruising speed: 220km/h, service ceiling: 3000m, range with 8,000kg payload: 420km, payload: 8000-12000kg
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Post by elangguntur on Sept 16, 2008 11:51:08 GMT 7
Proyek Mi V-16 tahun 1967, hanya proposal..kebayang kalo jadi....dasar russia..edun.
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Post by elangguntur on Sept 16, 2008 11:53:59 GMT 7
Mil Mi-46T Mi-46T TYPE: Twin-turboshaft passenger/freight transport helicopter. PROGRAMME: Project announced summer 1992; no further announcements. DESIGN FEATURES: Replacement for Mi-6, with T-O weight just over half that of Mi-26. General configuration similar to Mi-26; seven-blade main rotor, five-blade tail rotor; non-retractable tricycle landing gear with twin wheels on each unit; few windows in hold; rear-loading ramp and doors; engines above hold, forward of main rotor driveshaft.
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Post by elangguntur on Sept 16, 2008 11:59:08 GMT 7
Heli buatan Yakovlev, Yak-60 di luncurkan tahun 1960, sayang hanya sebatas konsep. Ini juga edan kalo dulu bener2 di buat, nggak kira2, dua kali Boeing CH-46. Technical data for Yak-60 Rotor diameter: 35m, fuselage length: 46m, take-off weight: 100,000kg, empty weight: 55,000kg
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masdwi
Angkasa members
Posts: 40
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Post by masdwi on Sept 16, 2008 12:35:00 GMT 7
Kalau bisa sih memang punya 1 Ska Heli angkut berat dengan Mi-26. Tapi kalau kelewat mahal ya mungkin dah cukup dengan 4 Ska Cougar / Mi-17.
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Post by dakota64 on Sept 20, 2008 9:32:12 GMT 7
Mas kalau mau cari buku Segesit Puma Sekuat Gajah dimana, barangkali bisa carikan nanti diganti harga plus ongkirnya....saya tinggal dijogja...thank's
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