Flight: 3-31-52
Date: July 30, 1964
Pilot: Capt. Joe Engle
Launch: Hidden Hills on magnetic heading 230°, MH-96 Adaptive, R.C. "OFF," BCS "OFF," Heading vernier to "Standby," Ventral off.
Launch Point Coordinates: 35° 55' N, 115° 09' W
1. Launch, light engine, increase to 100% T. Rotate at 10° a until q = 20°.
2. q = 20° - maintain q = 20°.
3. Pushover to O "g".
4. Reduce to minimum thrust.
5. Modulate speed brakes (» 35°) to maintain slow longitudinal acceleration. Increase a to maintain H = 78,000 ft.
6. Burnout. Maintain H = 78,000 ft.
7. Roll to » 70° left bank, increase a to 10°, maintain H-dot » O. (g » 3.0)
8. Pushover to a » 4°, roll to » 60° right bank, increase a to 10°. Turn to high key heading of » 225°.
9. Pushover to a » 4°, roll level, retract speed brakes, descend at » 400 fps.
10. Abeam Cuddeback, vector to high key, speed brakes as required, Engine Master Off.
ll. High Key.
2. X-15 radios - I never did get 279.9 from Beatty. Once, within 5 minutes of launch, NASA-l was coming in pretty fuzzy.
3. APUs - The APUs worked real good.
4. Damper system - Dampers worked real good.
5. Flow direction sensor - Ball nose worked real good.
6. Launch space positioning - It was good.
7. Launch transients (q, f, y) - Pitch, roll and yaw were all minimal.
8. Engine start - Engine start was normal, I guess.
9. Unforeseen incidents - None.
2. Heating run (V » 4800, H » 77,000, 0 < a < 3°) - Everything was normal.
3. Controllability during heating run - No real problem.
4. Rate control task - q 2 1/2 , f 2 , y 1 1/2 .
5. Altitude profile versus simulator - Evidently, it was pretty close. I think I got faked out on the rate of climb and I started to push-over early on that. But, all the rest of the instruments for cross-check that we had, and had been using on the simulator, brought us back to profile and q parameters pretty close.
6. Unforeseen incidents - Nothing unforeseen in that area.
2. Glide energy management versus simulation - I arrived over Cuddeback with more energy than what I had expected from simulation, but I had come in from Cuddeback at that energy condition enough times that there wasn't any real problem. I had a pretty good idea what to do.
3. Approach and landing - It was made with high energy
and touchdown was about 205 knots indicated. I kept easing forward on the
stick during slide-out and then made some pitch inputs, and could feel
the difference in deceleration on the airplane. (Did you have a little
pitch down trim?) I'd rolled in about 1-1/2° on the side dial, nose
down. I'd rolled it in I think about high key and when he called, I rechecked
it. (Did you hold a little aileron before launch?) Yes. Just about enough
to take out the slack is all. 1/2" on the center stick.
During this maneuver I'd rate the ·a control as shown above. (Any other comments about control features?) I would have guessed a lower rating for the center stick from the simulator, because it seemed easier to fly in the simulator. But, in the airplane, it seemed like it took more attention to fly it with center stick than with side stick. Maybe it was because I had been flying with the side arm and then switched over to the center stick.
2. ·q control P.R. in pitch (a control only) center stick q 3, side stick q 3
This would be during the energy management home. I made some little changes in pitch just to see how hard it was to go from one a to another a and I'd rate them as shown above under these conditions. (Did you fly q on the ball?) I was flying an a, come to think of it, because I could read it out closer there. So actually that's another a rating. (Later in the flight where you had wings level?) Right.
3. ·f control P.R. in roll center stick f 3, side stick f 3
The ratings are shown above. (You couldn't tell any difference in response?) No, it seemed about the same. I wasn't maintaining a particular roll angle for very long. I set up a roll angle and saw what H was doing and adjusted the roll angle accordingly and so it was kind of a transient, or rather a changing roll angle a11 the time. (Is there any reason why you wouldn't fly center stick for roll maneuver?) No. There seems to be a little more effort involved using center stick. There is more movement connected with it and with the pressure suit, you notice the movement more than you would in the simulator, whereas on the side arm it's just a wrist action. (Did you try any lateral control?) No.
4. Deflection/An trim follow-up feature - In the initial turn, as I said before, it felt like I had a good deal of stick deflection in. I had rolled in some pitch rate command on the side arm controller, but I didn't look down to see how much I'd rolled in so I was a little bit leery about fanning in some more until I saw what the airplane was going to do. This probably was the reason for the slow establishing of a. (Did you hold any appreciable forces while you were rolling trim in?) Yes, I would say so. I didn't have enough pitch rate trimmed in initially and I had to go back and trim some more and it felt like a pretty good force on the side arm. (Could you tell that the trim followed?) I'm pretty sure it did. (Was there a definite lag here?) Yes, the force was high at first and then it would start bleeding off.
5. Deadband, breakout force - I'd say that's pretty much negligible.
6. Overcontrol, P.I.O. tendency - There weren't any tendencies to overcontrol or get into P.I.O. The overshoot on q was a result of diverted attention more than not being able to stop q. I was on side stick there.
7. Longitudinal acceleration effect - I think we pretty well covered that too.
8. Deflection ratio between pitch and roll control Well,
it seemed that there was a pretty good deflection to establish this initial
10° a. Roll never has seemed to take very
much deflection in this airplane. I am real hesitant to compare the first
turn to the second turn, I don't think there is any real good comparison.
q 4 , f 2 1/2 , y 1 1/2 .
The most adverse piloting task was establishing the a on the initial turn and I'll rate it as shown above. (Did you watch longitudinal acceleration?) I thought I hesitated on putting out speed brakes because I came back on the throttle and may have looked at longitudinal acceleration then and seen a good healthy positive g. I looked down while I was pulling the speed brakes about half way out to make sure I still had positive acceleration before putting speed brakes all the way out. After they were out I didn't look at it again. I was concentrating pretty much on holding altitude and it's far enough out of the scan pattern that it's a little difficult to look down there and look back up and keep correlating around the fast scan. (Did it look like you can control it pretty accurately?) I think you could.
(What is your comparison between SAS and MH-96?) I like
to fly the MH-96 better, I think. There are certain flight conditions that
you try and establish that SAS is easier to set-up for, like a zero g burn
profile for example. You can go right to zero on the trim and you are pretty
well sure you've got zero g and you can leave it there. On the Honeywell
you have to keep adjusting even once you've established the zero g flight
trajectory. The same thing on setting up an angle of attack. You can trim
it in on SAS and set it and you have to do very little adjusting. It seems
like you have to keep adjusting with MH-96. The adjustment task is low
but you still have to keep adjusting, you can divert your attention more
on SAS but overall on a flight like this one today where things are changing
pretty much all through the profile anyway, I think MH-96 is a lot easier
to fly. Didn't seem to be any problem landing. I think you can pretty much
launch hands off. I had a little bit of side deflection in and no back
deflection and it came up like in the simulator. It comes up on 5°
a right away.