SAWE Report - Cal Poly San Luis Obispo

Table 11.X - Landing Results
Weight
124,800 lb (56,610 kg)
Maximum lift coefficient 1.2
Stall speed 242 ft/s (73.7 m/s)
Takeoff speed 266 ft/s (81.1 m/s)
50 ft obstacle speed ≥ 290 ft/s (88.4 m/s) 294 ft/s (89.6 m/s)
Dry braking friction coefficient 0.3
Icy braking friction coefficient 0.1
Thrust reverser effectiveness
25% Mil.
Dry runway length 3,857 ft (1,176 m)
Dry field length over 50 ft obstacle 5,256 ft (1,602 m)
Icy runway length 5,707 ft (1,739 m)
Icy field length over 50 ft obstacle 7,107 ft (2,166 m)
11.6 Performance Summary
As shown above, the Vendetta meets all performance requirements in the RFP. A summary of
the performance requirements is shown in Table 11.XI.
Table 11.XI - Performance Summary
Requirement
Value
Supercruise Mach Number 1.6 1.6
Supercruise Mission Radius 1,750 nm (3,240 km) 1,750 nm (3,240 km)
Dash Altitude > 50,000 ft (15,240 km) > 54,000 ft (16,460 km)
1g Mil. Ps M = 1.6, 50,000 ft 0 ft/s (0 m/s) 95.7 ft/s (29.2 m/s)
1g Max. Ps M = 1.6, 50,000 ft 200 ft/s (61.0 m/s) 316 ft/s (96.3 m/s)
2g Max. Ps M = 1.6, 50,000 ft 0 ft/s (0 m/s) 108 ft/s (32.9 m/s)
Max. Turn Rate M = 0.9, 15,000 ft 8 deg/s 13.1 deg/s
Takeoff Field Length 8,000 ft (2,438 m) 5,280 ft (1,609 m)
Landing Field Length 8,000 ft (2,438 m) 7,107 ft (2,166 m)
Fuel Burn Over Mission ─ 57,940 lb (26,280 kg)
Maximum Mach Number at 36,000 ft ─ 2.1
81