ATP-5-0-2-1 Staff Reference Guide Volume 1 Download

Movement and Maneuver Planning Factors 07 December 2020 ATP 5-0.2-1 223 Obstacle A B C D E F G H I J K Country and vehicle Water Fording (m) Height to Clear (m) Width to clear (m) Max Gap to Travers e (m) Ground Clearance (m) Max Step (m) Max Tile (m) Max Gradient (%) Max Strattle (%) Ground Pressure (pbi) Depression and Elevation (degrees) U.S. M1 1.22 2.89 3.6 2.74 0.48 1.24 40 60 2.14 13.4 -10+20 U.S. M2/M3 2.92 3.04 2.54 0.45 0.91 40 60 1.87 11.8 +30-20 (TOW) +60-10 (25mm) U.S. Stryker 1.35 3.2 2.87 1.98 0.53 0.60 30 60 2.94 63 psi (soil) -20+60 RWS U.S. Paladin 1.07 3.63 3.3 1.83 0.45 0.60 0.53 60 2.38 13.6 -11.45 +76.37 U.K. Centurion 1.2 2.96 3.4 3.35 0.51 0.9 30 60 2.19 13.3 -10+20 U.K. Chieftain 1.07 2.9 3.66 3.15 0.51 0.91 30 60 2.44 11 -10+20 GER Leopard 2 2.25 2.93 3.71 3 0.48 1.15 30 60 2.15 12.2 -9+20 FRA AMX-30 2 2.86 3.1 2.9 0.45 0.93 30 60 1.96 10.9 -8+20 Figure D-1. Friendly vehicle movement planning factors AIRCRAFT D-3. Material in this section is derived from ATP 3-01.81, FM 3-04, and GTA 55-07-003. Tables D-11 through D-16 on pages 224–226 show selected aircraft characteristics, fuel consumption, loads, and airspeed conversions. Table D-17 on page 226 describes types of unmanned aerial systems. Table D-18 on page 227 shows planning factors for assembly areas.