Kawasaki P-1

Airplanes

Length

38 m

Flat Wing Span

35.4 m

Height

12.1 m

Cruise Speed

833 km/h

Max Speed

996 km/h

Max Ceiling

13520 m

Number of Engines

First Flight

2007-09-28

Entry Into service

2013-01-01

Maximum Take-Off Weight

79.7 t (paragliders: kg)

Maximum Range

8000 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Kawasaki P-1	79.7	8000

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Tupolev Tu-110	Lyulka AL-7	38.3	37.5	100	Compare
Hawker Siddeley Nimrod	Rolls-Royce Spey	38.4048	34.7472		Compare
British Aerospace Nimrod AEW3	Rolls-Royce Spey	41.7576	35.052		Compare
Vickers Vanguard	Rolls-Royce Tyne	37.1856	35.9664	139	Compare
Lockheed P-7	General Electric GE38	34.1376	32.3088		Compare
Boeing XB-55	Allison T40	35.9664	41.148		Compare

All data (23 fields)

Name: Kawasaki P-1
Manufacturer: Kawasaki Heavy Industries
Description: The Kawasaki P-1, previously P-X and XP-1, is a Japanese maritime patrol aircraft developed and manufactured by Kawasaki Aerospace Company.
ICAO Code: P1
First Flight: 2007-09-28
Entry Into service: 2013-01-01
Designer: Kawasaki Heavy Industries
Type: Maritime patrol aircraft
Length (m): 38
Height (m): 12.1
Cockpit Crew: 3
Max Speed (km/h): 996
Cruise Speed (km/h): 833
Max Ceiling (m): 13520
Armament: 8, 2x on each wing and 2x on each wing root. Eight internal bomb bay stations
National Origin: Japan
Powerplant Description: 4 × IHI F7-10 turbofan engines, 60 kN thrust each
Primary Users: Japan Maritime Self-Defense Force
Status: In service (36)
Wikipedia Article (URL): en.wikipedia.org/wiki/Kawasaki_P-1
Flat Wing Span (m): 35.4
Wake Category: M
Number of Engines: 4