FlightGlobal.com
Home
Premium
Archive
Video
Images
Forum
Atlas
Blogs
Jobs
Shop
RSS
Email Newsletters
You are in:
Home
Aviation History
2002
2002 - 2508.PDF
Directory: military helicopters Manufacturer Model Kamov Ka-32A Helix C Ka-29133 special forces MD Helicopters MD520N MD Explorer NH Industries NH90TTH NH90 NTH similar PZL-Swidnik Mi-2 Hoplite Powerplant 2x1,645kWKIimov TV3-117VMA Fuse length (m) Height (m) MTOW (kg) Max int load (kg) Max op ceiling (ft) Max speed (kt) Over length (m) Main rotor di (m) OEW (kg) 10 36 11.30 5.49 15.90 helicopter and Ka-31 airborne eariy warning machine similar 1 x 336kW R-R 250-C20R 2x410kWPWC PW207E 2x1,788kWR-R Turbomeca RTM322 2x1,788GE T700-T6E 2 x 315kW PZL- Rzeszow GTD-350 7.77 9.80 9.86 11.84 16.14 16.83 11.94 17.42 Mil has proposal for Turbomeca Arrius 2F Mi2, MTOW 3.700kg. load 1 Kama W-3ASokol NAVAL AgustaWestland Sea King Super Lynx 300 Kaman SH-2G Super Seasprite Kamov Ka-27/Ka-28 Helix Mil Mi-14Haze Sikorsky MH-60R Seahawk 2x315kWR-R 250-C20B 2 x 660kW PZL- Rzeszow PZL-10W 2x1.120kWR-R Gnome H1400-1T 2x1,210kWLHTEC CTS800-4N 2x1,283kWGE T700-401 2x1,635kWKIimov TV3-117VMA 2x1,270kWKIimov TV3-117 2x1.340kWGE T70O401C 12.03 17.42 14.21 18.79 17.20 22.15 13.33 15.24 12.00 16.00 11.30 12.25 18.40 25.32 15.24 19.77 Formerly SH-60R. US Navy replacement for SH-60B and SH-60F MH-60S Seahawk 2x1.340kWGE T700-401C 15.24 19.77 2.90 8.30 3.66 10.34 5.22 16.30 3.74 14.56 11.000 5.443 1.746 719 3,130 1,532 10.600 5,500 3,550 2,410 Max ext load (kg) Range (km) 4,000 5,000 800 1,027 1.417 1.600 4.500 4,000 700 800 550kg. max speed 127kL eight passengers 3.74 14.56 4.20 15.70 5.13 18.90 3.67 12.80 4.09 13.41 5.40 15.90 6.93 21.30 5.10 16.36 3.79 16.36 Formerly CH-60S naval utility machine, US Navy replacement for HH-60F Bell Helicopter Textron OH-58D Kiowa Warrior 1 x 485kW R-R T703-700 Kawasaki Heavy Industries OH-1 TRAINING Bell Helicopter Textron TH-67 Creek Mil Mi-34C 2 x 595kW Mitsubish MG5 1 x 315kW R-R 250-C20J 1 x 335kW R-R 250-C20R/4 1x245kWOKBM M-14V-26 piston 10.50 12.85 12.00 9.50 11.82 8.85 11.40 Proposal for Turbomeca Arrius 2C-powered Mi-34A 3.93 10.60 3.80 11.50 2.90 10.20 2.75 10.00 3,550 2,000 6,400 3,850 9,707 5,447 5,330 3.656 6,115 4.017 12.600 • 14,000 8.900 10.24 6.990 10.670 6.265 2,497 1,497 3,500 2,500 1,520 772 1,450 950 1,200 1.200 2.100 2.100 3,692 4,260 1,674 1,360 2,296 1,812 5,000 - 5,100 3,300 2,724 2,497 2.724 998 998 n/a 1.000 750 750 500 0 19,680 800 20.000 378 20.000 302 . 960 13.115 580 13.115 435 19.680 761 10,000 1,482 12,000 987 20,400 1,000 17,100 800 11.500 1.135 14,300 - 10,000 370 12,000 497 400 13,500 676 1,395 420 HIGE (ft) Std fuel (litre) Max crew I Cruise speed (kt) HOGE (ft) Aux fuel (litre) Max pax 140 130 152 128 140 139 175 162 113 103 113 103 140 134 113 122 160 137 141 136 146 135 125 116 145 126 152 120 125 114 156 146 130 115 110 92 11,480 3,700 12,800 9,400 15,300 14,000 9.514 5,413 5,250 2.950 8.200 4,510 18,680 15,810 5,600 3,500 6,900 4,750 17,600 14.600 16.400 11,820 . 23,500 22,000 10,000 6,900 - 12.800 8.800 4,920 2,950 2,180 1,270 242 600 - 2,470 600 476 600 422 1,720 0 3,714 863 985 882 1.045 760 4.470 3,800 450 2 13 1 5 2 5 4 20 2 7 2 9 3 13 2 28 2 9 3 8 3 12 3 18 2.245 910 2.245 910 424 0 - 160 314 0 165 0 3 3 - 2 0 2 n/a 3 4 2 3 32 20-26 AUGUST 2002 FLIGHT INTERNATIONAL www.flightinternational.com
Sign up to
Flight Digital Magazine
Flight Print Magazine
Airline Business Magazine
E-newsletters
RSS
Events