4 × Ishikawajima-Harima / General Electric T64-IHI-10J turboprop engines, 2,605 kW (3,493 hp) each
Rate of Climb (ft/min)
1,601.0 ft/min @ MTOW/2,339.2 ft/min at 36,000 kg
Service Ceiling (ft)
7,195 m @ MTOW/8,655 m @ 36,000 kg
Military/Afterburner Speed (kt)
276 kt
Cruise Speed (kt)
230 kt
Supercruise
No
Ferry Range (nm)
Max range: 2,061 nm @ 230 kn/ at 3,050 m
Endurance (min)
unknown
Takeoff / Landing Distance (m)
see below
Fuel Capacity (kg)
1,640 L usable fuel in 5x wing tanks + 10,849 L usable fuel in 2x fuselage tanks
Sensors
APS-80N Ocean search radar
Mounts
none
Loadout Options
SAR
Comms/Datalinks
Unknown. Assuming typical military comms
Aircraft Codes
Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles)
Comments
Take-off distance to 15 m (49 ft): 655 m (2,149 ft) 30° flap, BLC on, on land
Landing distance from 15 m (49 ft): 810 m (2,657 ft) 40° flap, BLC on, on land
Take-off distance: 555 m (1,821 ft) at 45,000 kg (99,208 lb) 40° flap, BLC on, on water
Landing distance: 220 m (722 ft) at 36,000 kg (79,366 lb) 60° flap, BLC on, on water
1 × Ishikawajima-Harima / General Electric T58-IHI-10-M2 turbo-shaft compressed air generator driving a C-2 compressor
DB Selector
Both
Baseline
none
Hypothetical
No
Name
Shin Meiwa PS-1/US-1/US-1A
Country
Japan
Service
JMSDF
In Commission
1971(PS-1) - 2017
Number in Service
PS-1: 23/US-1: 6/US-1A: 14
Length (m)
33.46
Wingspan (m)
33.15
Height (m)
9.95
Empty Weight (kg)
23 300
Maximum Takeoff Weight (MTOW) (kg)
43,000 kg from water/45,000 kg from land
Payload Weight (kg)
unknown
Crew
7
Propulsion
4 × Ishikawajima-Harima / General Electric T64-IHI-10J turboprop engines, 2,605 kW (3,493 hp) each
Rate of Climb (ft/min)
1,601.0 ft/min @ MTOW/2,339.2 ft/min at 36,000 kg
Service Ceiling (ft)
7,195 m @ MTOW/8,655 m @ 36,000 kg
Military/Afterburner Speed (kt)
276 kt
Cruise Speed (kt)
230 kt
Supercruise
No
Ferry Range (nm)
Max range: 2,061 nm @ 230 kn/ at 3,050 m
Endurance (min)
unknown
Takeoff / Landing Distance (m)
see below
Fuel Capacity (kg)
1,640 L usable fuel in 5x wing tanks + 10,849 L usable fuel in 2x fuselage tanks
Sensors
APS-80N Ocean search radar
Mounts
none
Loadout Options
SAR
Comms/Datalinks
Unknown. Assuming typical military comms
Aircraft Codes
Night Navigation (Ferry, Air-to-Air, Air-to-Surface Missiles)
Comments
Take-off distance to 15 m (49 ft): 655 m (2,149 ft) 30° flap, BLC on, on land Landing distance from 15 m (49 ft): 810 m (2,657 ft) 40° flap, BLC on, on land Take-off distance: 555 m (1,821 ft) at 45,000 kg (99,208 lb) 40° flap, BLC on, on water Landing distance: 220 m (722 ft) at 36,000 kg (79,366 lb) 60° flap, BLC on, on water 1 × Ishikawajima-Harima / General Electric T58-IHI-10-M2 turbo-shaft compressed air generator driving a C-2 compressor
Sources
https://en.wikipedia.org/wiki/Shin_Meiwa_US-1A https://simpleflying.com/shin-meiwa-stol-aircraft-story/ https://www.airvectors.net/avps1.html#m2 https://www.seaforces.org/marint/Japan-Maritime-Self-Defense-Force/AIRCRAFT/ShinMeiwa-US-1.htm