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.
 |