Tuntunan Menurut Al Quran dan Hadist Shahih: Mi-35 dan Mi-17 Helicopter Specifications

The Mil Mi-24 (Russian: Миль Ми-24; NATO reporting name: Hind) is a large helicopter gunship, attack helicopter and low-capacity troop transport with room for eight passengers.^[1] It is produced by Mil Moscow Helicopter Plant and has been operated since 1972 by the Soviet Air Force and its successors, along with more than 30 other nations.

In NATO circles, the export versions, Mi-25 and Mi-35, are denoted with a letter suffix as "Hind D" and "Hind E". Soviet pilots called the Mi-24 the "flying tank" (летающий танк; letayushchiy tank), a term used historically with the famous World War II Soviet Il-2 Shturmovik armored ground attack aircraft. More common unofficial nicknames were "Crocodile" (Крокодил; Krokodil), due to the helicopter's camouflage scheme and "Drinking Glass", (Стакан; Stakan) because of the flat glass plates that surround the Mi-24's cockpit.^[2]

Mi-24/Mi-25/Mi-35

Russian Mi-24PN
Role	Attack helicopter with transportcapabilities
National origin	Soviet Union/Russia
Manufacturer	Mil
First flight	19 September 1969
Introduction	1972
Status	In service
Primary users	Russian Air Force ca. 50 other users (see Operators section below)
Produced	1969–present
Number built	2,300 (estimated)
Developed from	Mil Mi-8

General characteristics

Crew: 2–3: pilot, weapons system officer and technician (optional)
Capacity: 8 troops or 4 stretchers or 2400 kg (5,291 lb) cargo on an external sling
Length: 17.5 m (57 ft 4 in)
Rotor diameter: 17.3 m (56 ft 7 in)
Wingspan: 6.5 m (21 ft 3 in)
Height: 6.5 m (21 ft 3 in)
Disc area: 235 m² (2,530 ft²)
Empty weight: 8,500 kg (18,740 lb)
Max. takeoff weight: 12,000 kg (26,500 lb)
Powerplant: 2 × Isotov TV3-117 turbines, 1,600 kW (2,200 hp) each

Performance

Maximum speed: 335 km/h (208 mph)
Range: 450 km (280 miles)
Service ceiling: 4,900 m (16076 ft)

Armament

Internal guns

flexible 12.7 mm Yakushev-Borzov Yak-B Gatling gun on most variants. Maximum of 1,470 rounds of ammunition.
fixed twin-barrel GSh-30K on the Mi-24P. 750 rounds of ammunition.
flexible twin-barrel Gryazev-Shipunov GSh-23L on the Mi-24VP and Mi-24VM. 450 rounds of ammunition.
PKB passenger compartment window mounted machine guns

External stores

Total payload is 1,500 kg of external stores.
Inner hardpoints can carry at least 500 kg
Outer hardpoints can carry up to 250 kg
Wing-tip pylons can only carry the 9M17 Phalanga (in the Mi-24A-D) or the 9K114 Shturm complex (in the Mi-24V-F).

Bomb-load

Bombs within weight range (presumably ZAB, FAB, RBK, ODAB etc.), Up to 500 kg.
MBD multiple ejector racks (presumably MBD-4 with 4 × FAB-100)
KGMU2V submunition/mine dispenser pods

First-generation armament (standard production Mi-24D)

GUV-8700 gunpod (with a 12.7 mm Yak-B + 2 × 7.62 mm GShG-7.62 mm combination or one 30 mm AGS-17)
UB-32 S-5 rocket launchers
S-24 240 mm rocket
9M17 Fleyta (a pair on each wingtip pylon)

Second-generation armament (Mi-24V, Mi-24P and most upgraded Mi-24D)

UPK-23-250 gunpod carrying the GSh-23L
B-8V20 a lightweight long tubed helicopter version of the S-8 rocket launcher
9K114 Shturm in pairs on the outer and wingtip pylons

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Mi-17

The Mil Mi-17 (NATO reporting name "Hip") is a Russian helicopter in production at two factories in Kazan andUlan-Ude. It is known as the Mi-8M series in Russian service. It is a medium twin-turbine transport helicopter. There are also armed gunship versions.

Mi-17 / Mi-8M

A Mi-17 from the Afghan Air Force takes off from Kabul International Airport
Role	Transport helicopter
National origin	Soviet Union
Design group	Mil Moscow Helicopter Plant
Built by	Kazan Helicopter Plant
First flight	1975
Introduction	1977 (Mi-8MT), 1981 (Mi-17)
Status	In service
Primary users	Russia ca. 60 other countries
Produced	1977–present
Number built	about 12,000^[1]
Unit cost	Prices vary based on specifications (military and civilian prices differ)
Developed from	Mil Mi-8

General characteristics

Crew: Three – two pilots and one engineer
Capacity: 30 troops or 12 stretchers or 4,000 kg (8,820 lb) cargo internally /5,000 kg (11,023 lb) externally slung.
Length: 18.465 m (60 ft 7 in)
Rotor diameter: 21.25 m (69 ft 10½ in)
Height: 4.76 m (15 ft 7¼ in)
Disc area: 356 m² (3,834 ft²)
Empty weight: 7,489 kg (16,510 lb)
Loaded weight: 11,100 kg (24,470 lb)
Max. takeoff weight: 13,000 kg (28,660 lb)
Powerplant: 2 × Klimov TV3-117VM turboshafts, 1,633 kW (2,190 shp) each