Northrop M2-F2

USA


Description:


M2-F2 in flight

M2-F2 on the ramp at the NASA Dryden Flight Research Center.

M2-F2 diagramme


Technical Data:

Manufacturer:Northrop
Operator:US
Length :22 ft 2 in (6.76 m)
Wingspan:9 ft 8 in (2.94 m)
Heigh:9 ft 6 in (2.89 m)
Wing area:160 ft² (14.9 m²)
Empty weight:4,620 lb (2,095 kg)
Loaded weight:6,000 lb (2,722 kg)
Max takeoff weight:7,485 lb (3,395 kg)
Crew:one pilot
Power: 1 × Reaction Motors Upgraded XLR-11 four-chamber
rocket engine, 8,000 lbf (36 kN)
Thrust:
Max speedt:Mach 0.707 (466 mph, 750 km/h)
Range:8.6 nm (10 mi, 16 km)
Service ceiling:45,000 ft (13,700 m)
Wing loading: 43.2 lb/ft² (196 kg/m²)
Developed fromNASA M2-F1
First Flight12 July 1966
Last Flight10 May 1967
Total Flights
Fastest Flight
Highest Flight
StatusRebuilt as M2-F3.

Aircraft serial number: NASA 803, 16 unpowered flights.

Testing:

M2-F2 pilots:


Launch list M2-F2 flights:

Vehicle
Flight #
Date Pilot Mach Velocity
(km/h)
Altitude
(m)
Duration Comments
M2-F2 #1 July 12, 1966 Thompson 0.646 727 13,716 00:03:37 First M2-F2 Flight. Unpowered glide. 320 km/h landing.
M2-F2 #2 July 19, 1966 Thompson 0.598 634 13,716 00:04:05 Unpowered glide. Determination of lateral stability control, longitudinal trim, vehicle performance and landing characteristics.
M2-F2 #3 August 12, 1966 Thompson 0.619 692 13,716 00:04:38 Unpowered glide. Determine effect of increasing Mach number, minimum damper requirements, testing of longitudinal and lateral stability and control.
M2-F2 #4 August 24, 1966 Thompson 0.676 718 13,716 00:04:01 Unpowered glide. Determine control damper requirements, lift-drag ratio, elevon response, flap effectiveness and longitudinal stability and control.
M2-F2 #5 September 2, 1966 Thompson 0.707 750 13,716 00:03:46 Unpowered glide. Evaluate 360 degree overhead approach, determine control damper-off handling qualities.
M2-F2 #6 September 15, 1966 Peterson 0.705 750 13,716 00:03:30 Unpowered glide. Pilot checkout.
M2-F2 #7 September 20, 1966 Sorlie 0.635 678 13,716 00:03:31 Unpowered glide. Pilot checkout.
M2-F2 #8 September 22, 1966 Peterson 0.661 702 13,716 00:03:53 Unpowered glide. Longitudinal and lateral stability and control with dampers.
M2-F2 #9 September 28, 1966 Sorlie 0.672 713 13,716 00:03:53 Unpowered glide. Complete pilot checkout and extend flight envelope.
M2-F2 #10 October 5, 1966 Sorlie 0.615 692 13,716 00:03:45 Unpowered glide. Explore lateral and longitudinal stability and control characteristics with dampers on and off.
M2-F2 #11 October 12, 1966 Gentry 0.662 702 13,716 00:03:54 Unpowered glide. Pilot checkout.
M2-F2 #12 October 26, 1966 Gentry 0.605 642 13,716 00:03:47 Unpowered glide. Obtain stability and control data at 7 and 11 degree attack angles and upper flap effectiveness.
M2-F2 #13 November 14, 1966 Gentry 0.681 716 13,716 00:04:21 Unpowered glide. Test stability and control, determine vehicle performance characteristics.
M2-F2 #14 November 21, 1966 Gentry 0.695 735 13,716 00:03:50 Unpowered glide. Test stability and control, determine vehicle performance characteristics.
M2-F2 #15 May 2, 1967 Gentry 0.623 661 13,716 00:03:51 Unpowered glide.
M2-F2 #16 May 10, 1967 Peterson 0.612 649 13,716 00:03:43 Unpowered glide
Crash landing.

External links:


Astrophilately covers:

Flight 5 - Pilot Thompson. Credit: #412



Ref.: Ref: #53, #98, #412 - update: 09.08.20 Home