Flight No.: 1-28-49 Date of Flight : 5/22/62
Pilot: Major Robert Rushworth
Subject of Test: Local flow investigation.
Airplane Configuration: Basic X-15.
Launch: Hidden Hills
on a magnetic heading of 226, ASAS armed.
No. | Time | Alt | V | a | Event |
1. | 0 | 45 | 790 | - | Launch, light engine, increase to 100%, rotate until 2 g's is attained. |
2. | 29 | 50 | 1900 | 9 | Maintain 2 g until q = 30°. |
3. | 37 | 58 | 2350 | 5 | Pushover to a = 0° |
4. | 67 | 84 | 4300 | 0 | Extend speed brakes |
5. | 77 | 90 | 5200 | 0 | Shutdown |
6. | 83 | 90 | 5050 | 0 | Increase a in 5° increments to 10° |
7. | 102 | 87 | 4700 | 10 | When q = +10° decrease a in 5° increments to 0° |
8. | 127 | 79 | 4050 | 0 | When q = -10° increase a in 5° increments to 10° |
9. | 149 | 68 | 3400 | 10 | When q = +10° decrease a in 5° increments to 0° |
. | |||||
10. | 164 | 63 | 2600 | 0 | When q = -10° increase a in 5° increments to 10° |
11. | 175 | 60 | 2100 | 10 | Push over to 1g |
12. | Vector to High Key, retract speed brakes, jettison, H2O2 OFF. | ||||
13. | Check ventral armed, pressurize tanks. | ||||
14. | Before APU shutdown, cycle controls, retract flaps, set stabilizer to zero, push-to-test ball nose - data OFF. |
Flight No. 1-28-49
NOTES:
2. q vernier will be set at 30°, a crosspointer will null at 0°.
3. Emergency lakes, Three Sisters and Cuddeback.
2. Malfunction of inertial platform attitudes.
3. Malfunction of ball nose.
2. If ball nose fails proceed as planned using g increments instead of a to determine the pull-up maneuvers.
3. If total pitch or roll SAS fails, proceed as planned, do not exceed 8° a.
4. For inadvertent
engine shutdown: prior to 39 sec, return to Hidden Hills; 39 to 50 seconds,
proceed to Three Sisters; 50 to 65 seconds, proceed to Cuddeback; above
65 seconds, proceed to Edwards - two engine restarts may be attempted in
all cases.