Flight No.: 2-C-58 Scheduled Date : November 4, 1964
Pilot: John B. McKay
Purpose : Landing Gear Door Modification checkout after Cold Soak
Ground Track: As indicated on attached map
1. B-52 will make a normal takeoff and climbout to arrive at northwest edge of Rosamond Lake at approximately 30,000 feet. This will be 44 minutes to X-15 gear drop. B-52 will continue climb to 45,000 feet.
2. Flight will proceed according to modified X-15-2 Flight Check List. (Check List changes will be covered at Crew Briefing.)
3. At 4 minutes to gear drop, B-52 will begin descent to 30,000 feet. X-15 gear drop will be made at 30,000 feet with 250 KTS CAS.
4. After X-15 gear drop, proceed with modified Alternate Plan (No launch), B-52 vector to the downwind leg for landing.
Flight No.: 2-35-60 Scheduled Date : November 5, 1964
Pilot: John B. McKay
Purpose : To obtain data for the following programs:
2. Stability and control evaluation - (Glenn Robinson)
3. Star Tracker partial functional checkout - (Lovic Thomas)
Launch: Hidden Hills #2 on magnetic heading 235°, SAS Hi-Lo-Hi (8-4-8), ASAS Armed, heading vernier "Standby," both BCS "OFF," RAS "OFF."
Launch point coordinates:
35° 58 N; 115° 39 W.
No. | Time | Alt | V | a | q | Event |
1. | 0 | 45 | 790 | 0 | 145 | Launch, light engine, increase to 100%T. Rotate at 10° a (» 1.8g) until q = 20°. |
2. | 20 | 46 | 1700 | 10 | 630 | q = 20°. Maintain q = 20°. |
3. | 30 | 50 | 2000 | 5 | 760 | Extend speed brakes to 35°. |
4. | 52 | 64 | 2850 | 4 | 760 | Pushover to zero g. (H-dot » 800 fps). |
5. | 80 | 80 | 4500 | 0 | 880 | Shut down, retract speed brakes, increase a to » 4° to maintain 80,000 ft. |
6. | 88 | 80 | 4350 | 4 | 820 | Roll to » 60° left bank, increase a to » 8° (g = 2.0). Maintain g = 2.0 and H = 80,000 ft. |
7. | 106 | 80 | 4000 | 9 | 700 | Roll level (heading » 220°). Maintain H = 80,000 ft. Star Tracker switch to "Exp. On." |
8. | 119 | 80 | 3800 | 5 | 620 | Disengage ASAS, pitch damper "OFF," perform pitch pulse. Pitch damper "Hi." |
9. | 130 | 80 | 3600 | 5 | 570 | Set up rate of descent of » 250 fps. |
10. | 150 | 75 | 3400 | 5 | 650 | Yaw and roll dampers "OFF," perform rudder pulse. Roll "Lo," Yaw "Hi." |
11. | 167 | 71 | 3200 | 5 | 680 | Pitch damper "OFF," perform pitch pulse. Pitch damper "Hi." |
12. | 182 | 68 | 3000 | 5 | 700 | Cuddeback, extend speed brakes to 35°, increase rate of descent to » 400 fps. |
13. | 195 | 62 | 2600 | 3 | 700 | Yaw and roll dampers "OFF," perform rudder pulse. Roll "Lo," Yaw "Hi." |
14. | 209 | 57 | 2200 | 3 | 630 | Pitch damper "OFF," perform pitch pulse. Pitch damper "Hi," Arm ASAS, vector to High Key, speed brakes as required. |
15. | High Key - check flap and "squat" circuit breakers in. | |||||
16. | Before APU shutdown, cycle flaps, set stabilizer trim to zero, data off. |
Notes:
2. Emergency Lakes: Silver and Cuddeback.
3. Flight duration: Approximately 8 min.
4. Flight plan based on 58,700# thrust - engine #108
Total burn time at 100% = 83 sec.
Launch weight = 34,600#, burnout weight = 16,450#
(300# allowed for in-flight jettison check)
2. Malfunction of any SAS channel.
3. Malfunction of inertial platform.
4. Total ball nose
failure.
Failure Action
1. | Radio or Radar | Proceed as planned. | |
2. | Total Pitch Damper | Proceed as planned. Manipulate roll and yaw dampers at pilot's discretion. | |
3. | Total Yaw Damper | Proceed as planned except pushover to 2° a at 52 sec. instead of zero g. | |
4. | Total Roll Damper | Same as 3 except turn yaw damper "off." Manipulate pitch damper at pilot's discretion. | |
5. | Attitude Failure | Use 4 1/2° a in place of 20° q at 22 sec. | |
6. | Ball Nose | Rotate at 1.8g instead of 10° a. Do not disengage dampers. | |
7. | Delayed engine light | Pushover to zero g at H = 63,000 ft. (H-dot » 850 fps). |
8. Inadvertent engine shutdown
0 - 30 sec Hidden Hills
30 - 57 sec Silver (2000 fps)
57 - 64 sec Cuddeback (3000 fps)
64 - Up sec Edwards
(3400 fps)