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OVERVIEW
NORTHROP N-9M (NS-99)
1942
 
ENGINEERING RESEARCH AIRCRAFT
 
     
 
 
DATA
 
 
NORTHROP N-9M
 (N-9M-1, N-9M-2, N-9MA, & N-9MB)
CLASSIFICATION
CLASS :
 ENGINEERING RESEARCH AIRCRAFT
COUNTRY OF ORIGIN :
 UNITED STATES
MANUFACTURER :
 NORTHROP AIRCRAFT COMPANY, INC
FIRST FLIGHT :
 DECEMBER 27, 1942
SERVICE DELIVERY :
 NONE
NUMBER BUILT :
 4
   
SPECIFICATION
SPAN :
 17 ft 9 in (5.4 m)
LENGTH :
 60 ft 0 in (18.3 m)
HEIGHT :
 6 ft 7 in (2 m)
WING AREA :
 490 sq ft (45.5 m sq)
WEIGHT EMPTY :
 5,893 lb (2,673 kg)
WEIGHT LOADED :
 13,946 lb (6,326 kg)
WEIGHT MAX :
 --
POWER PLANT :
 2 x Menasco C6S-4 (1st 3 N-9M) Piston Engines, Rated at 260 hp ea;
 
 2 x Franklin XO-540-7 (N-9MB) Piston Engine, Rated at 260 hp
ARMAMENT :
 NONE
BOMB LOAD :
 NONE
CREW :
  1 - Pilot (Typical);
 
  2 - Pilot & Observer (N-9MB)
   
PERFORMANCE
MAXIMUM SPEED :
 258 mph (415 km/h)
CRUISING SPEED :
 208 mph
LANDING SPEED :
 --
CLIMB RATE :
 --
RANGE :
 500 miles (805 km); Endurance of 3.2 hrs
SERVICE CEILING :
 21,500 ft (6,553 m)
 
 
 
 
 
 
REFERENCES
 
 

Pape, Garry with John Campbell & Donna Campbell. The Flying Wings of Jack Northrop. Atglen, Pennsylvania: Schiffer Publishing, Ltd. 1994. ISBN 0-88740-597-5.

Pape, Garry and John Campbell. Northrop Flying Wings: A History of Jack Northrop's Visionary Aircraft. Atglen, Pennsylvania: Schiffer Publishing, Ltd., 1995. ISBN 0-88740-689-0.

Wooldridge, E. T. Winged Wonders: The Story of the Flying Wings. Washington, D.C.: Smithsonian Institution Press, 1983. ISBN 0-87474-966-2.

 
 
     
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