McDonnell Douglas YC-15

Airplanes

Length

37.9 m

Flat Wing Span

33.6 m

Height

13.2 m

Flat Wing Area

160 m²

Max Seating

150

Cruise Speed

872 km/h

Max Speed

950 km/h

Max Ceiling

9100 m

Number of Engines

Aircraft Engine

First Flight

1975-08-26

Number Built

Maximum Take-Off Weight

98.285 t (paragliders: kg)

Maximum Range

4800 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
McDonnell Douglas YC-15	98.285	4800

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Handley Page Victor		34.7472	33.528		Compare
Hawker Siddeley Nimrod	Rolls-Royce Spey	38.4048	34.7472		Compare
BAE Systems Nimrod MRA4	Rolls-Royce BR700	38.4048	38.7096		Compare
Vickers Vanguard	Rolls-Royce Tyne	37.1856	35.9664	139	Compare
Kawasaki P-1		38	35.4		Compare
Martin P7M SubMaster		41.4528	33.8328		Compare

All data (25 fields)

Name: McDonnell Douglas YC-15
Manufacturer: McDonnell Douglas
Description: The McDonnell Douglas YC-15 is a prototype four-engine short take-off and landing (STOL) tactical transport.
ICAO Code: C15
First Flight: 1975-08-26
Designer: McDonnell Douglas
Type: Tactical airlifter
Length (m): 37.9
Height (m): 13.2
Cockpit Crew: 3
Max Seating: 150
Max Speed (km/h): 950
Cruise Speed (km/h): 872
Max Ceiling (m): 9100
Capacity Description: Up to 150 troops or 78000 lb of cargo
National Origin: United States of America
Number Built: 2
Powerplant Description: 4 × Pratt & Whitney JT8D-17 turbofans, 72.5 kN thrust each
Status: Cancelled
Wikipedia Article (URL): en.wikipedia.org/wiki/McDonnell_Douglas_YC-15
Flat Wing Span (m): 33.6
Flat Wing Area (m²): 160
Wake Category: M
Aircraft Engine: Pratt & Whitney JT8D
Number of Engines: 4