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.
|