Rushworth: |
Both
BCS on. Data off. |
|
|
NASA
1: |
Chase
1, verify again that we have nothing coming from the prime line from the
rear of the airplane. |
|
|
Chase
1: |
It's
all dry. |
|
|
B-52: |
Coming
up on 11 minutes. |
|
|
Rushworth: |
Precool
is off. RAS auto is on. Bob, I want to verify that helium shutoff valve
switch is still closed at this point? |
|
|
NASA
1: |
Yes,
it 's on. |
|
|
Rushworth: |
Helium
shutoff is closed? |
|
|
NASA
1: |
OK. |
|
|
Rushworth: |
Does
that mean open or closed? |
|
|
B-52: |
10
minutes now. |
|
|
Rushworth: |
APU
cooling switch is normal. Both blowers are BLN2.
Pressure cooling is on. |
|
|
NASA
1: |
OK,
get your helium shutoff valve switch open. |
|
|
Rushworth: |
Roger,
open, checklist is wrong then. This back .......... I checked the ..........
doesn't go back on. 45,000 feet and 1000 fps, Jack. |
|
|
Russel: |
Roger,
reading 920 fps. |
|
|
Rushworth: |
a
and b
are displaced. Cabin source 3500. I have helium shutoff at 0900 on. |
|
|
B-52: |
9
minutes now. Preparing to turn at 8. |
|
|
Rushworth: |
#2
hyd. temp is -40. Data is on. 2 APU coming on. #l coming on. |
|
|
Chase: |
Looks
good. |
|
|
B-52: |
30
seconds to turn, confirm NASA 1, are we cleared to turn? |
|
|
NASA
1: |
Turn
at 8 minutes, right. |
|
|
Rushworth: |
My
hyd. pressures are 30 and 36, and I'm on alternators, engine is reset,
200 volts each side. |
|
|
B-52: |
8
minutes, starting turn. |
|
|
NASA
1: |
Roger.
Bob, check engine reset? I got your check engine reset, is that right? |
|
|
Rushworth: |
Affirmative.
Flaps coming down. |
|
|
Chase: |
Flaps
coming down. Up. |
|
|
Rushworth: |
All
back up. |
|
|
Chase: |
Full
up. |
|
|
Rushworth: |
I'm
trimmed to zero. |
|
|
Chase: |
It's
trimmed to zero out here. Cycling a little. |
|
|
Rushworth: |
Circuit
breakers are in, data is off. Mixing chambers are - #l about a -20, #2
is a -40. Aux cabin pressure switch is on. |
|
|
NASA
1: |
What's
your angle of attack indication? |
|
|
Rushworth: |
It's
3 right now in the turn. |
|
|
B-52: |
7
minutes. |
|
|
Rushworth: |
Do
you want to go platform internal in this turn? |
|
|
NASA
1: |
Go
ahead, Bob. |
|
|
Rushworth: |
OK
platform internal, fire ext auto, ASAS armed. |
|
|
Russel: |
Lube
oil temp 60°. |
|
|
NASA
1: |
You
got aux cabin pressure switch on, Bob? |
|
|
Rushworth: |
Affirmative. |
|
|
NASA
1: |
What's
your lox pump bearing temp? |
|
|
Rushworth: |
Its
still -53°. |
|
|
NASA
1: |
Was
the call -40° an error then? |
|
|
Rushworth: |
That
was mixing chamber temp. No, I guess that was a hyd. check that I gave
you that you thought was lox pump bearing. |
|
|
NASA
1: |
Still
-53°? |
|
|
Rushworth: |
Right. |
|
|
B-52: |
6
minutes. |
|
|
Russel: |
Lube
oil temp is up to 75 to 80° now. |
|
|
Rushworth: |
OK
SAS check is complete. SAS is re-engaged. ASAS is armed and gains
are 6-4-8. Stabilizer position should be the same. |
|
|
Russel: |
It's
the same, zero. |
|
|
Rushworth: |
2800
oxygen. |
|
|
B-52: |
5
minutes. |
|
|
Rushworth: |
I'm
on X-15 oxygen, cabin altitude 36,000 and cabin press is 3350. Ventral. |
|
|
Russel: |
Topoff
is about 30 seconds, Bob. |
|
|
Rushworth: |
OK,
no hurry. |
|
|
NASA
1: |
Russ,
continue around to 204° heading. |
|
|
B-52: |
Roger,
204°. |
|
|
NASA
1: |
Bob,
it looks like we're going to modify your last minute in time, the major
difference will be the igniter idle switch will not go on in 40 seconds
and we'll call this out for you. We're going to delay until 10 seconds,
be the old-fashioned start. |
|
|
Chase
2: |
Coming
up on the port side. |
|
|
B-52: |
4
minutes. |
|
|
Russel: |
Lox
topoff is complete. |
|
|
Rushworth: |
OK.
Data is on, calibrate, and pressurize. Control came back up to 600. Jettison
switches are jettison, both. Emergency lights are out. |
|
|
B-52: |
204°. |
|
|
Rushworth: |
And
I have about 48 pounds on each side. Data is off. Intercom switch is off,
how do you read? |
|
|
NASA
1: |
Loud
and clear. |
|
|
Rushworth: |
OK
I've got about 750 fps and 45,000 feet. APU bearing is still 53°. |
|
|
NASA
1: |
OK,
Bob, you are going to take the last minute at my count, OK? The functions
in the last minute. |
|
|
Rushworth: |
The
only change would be that I would hold igniter idle switch until after
the pump had started? |
|
|
NASA
1: |
Negative.
We will give you the count-down at 1 minute 40 seconds, 30 seconds, 10. |
|
|
B-52: |
3
minutes, 20 seconds ago. |
|
|
Russel: |
Platform
is in spec. |
|
|
Rushworth: |
I
got the 3 minute call. |
|
|
NASA
1: |
Russ,
go to 212°. |
|
|
Rushworth: |
Coming
up on 2 minutes, Bob? |
|
|
B-52: |
2
minutes now. |
|
|
Rushworth: |
Data
on, test ball nose, good test. I'm about 1° nose left on the needle
and a
showing about 2°, b
on 15. Cine is down, pulse. No head bumper. |
|
|
NASA
1: |
OK,
Bob, at one minute I'll pick up the count and advise you what to do, the
critical thing in the last minute will be the lox pump bearing temperature
as to whether we launch or not. |
|
|
Rushworth: |
Right. |
|
|
B-52: |
Coming
up on 1 minute now, launch master on. |
|
|
NASA
1: |
Prime
switch prime, Bob? |
|
|
Rushworth: |
Prime. |
|
|
NASA
1: |
Got
an igniter ready light? |
|
|
Rushworth: |
Got
.......... and all gages look good. Lox tank press has gone to 55, settling
back down. |
|
|
NASA
1: |
OK,
40 seconds, precool on now. |
|
|
Rushworth: |
Precool. |
|
|
Chase: |
Looks
good back here. |
|
|
NASA
1: |
Standby
at 30 seconds, I'll call pump idle. Pump idle now. |
|
|
Rushworth: |
Pump
idle. |
|
|
NASA
1: |
OK
call your manifold pressures. |
|
|
Rushworth: |
Manifold
pressures 350. |
|
|
NASA
1: |
Lox
pump bearing temperature? |
|
|
Rushworth: |
Coming
up now through 48 to 45 |
|
|
NASA
1: |
Lox
pump bearing temp? |
|
|
Rushworth: |
Coming
through 42. |
|
|
NASA
1: |
OK,
10 seconds now, go igniter idle. |
|
|
Rushworth: |
Igniter
idle. |
|
|
NASA
1: |
Follow
your chamber pressure? |
|
|
Rushworth: |
I
have igniter idle and looks good. |
|
|
NASA
1: |
How's
your lox pump bearing temp? |
|
|
Rushworth: |
35 |
|
|
NASA
1: |
Clear
to launch. |
|
|
Rushworth: |
3,2,1
launch. Good light? |
|
|
Chase: |
Good
light. |
|
|
Rushworth: |
SAS
is back on again, I got 10°. |
|
|
NASA
1: |
OK,
fine. Starting out on the track good. Coming up on 22 seconds now. |
|
|
Rushworth: |
It's
not my 20°. |
|
|
NASA
1: |
OK,
right on track, coming up on the profile, track is excellent. When you
get a chance right now, lox pump bearing temp please. |
|
|
Rushworth: |
-10.
Looks very good. |
|
|
NASA
1: |
Profile
is good, track is excellent. |
|
|
Rushworth: |
60
seconds, 60,000 feet. |
|
|
NASA
1: |
Roger,
very good. Time, coming up 65, 66, 67. |
|
|
Rushworth: |
OK,
I'm a little bit low. |
|
|
NASA
1: |
That's
right. |
|
|
Rushworth: |
On
heading now? |
|
|
NASA
1: |
Look
very good here, right on the profile and track is excellent. 86 seconds
now. |
|
|
Rushworth: |
Speed
brakes coming out now. 3250 manifolds. |
|
|
NASA
1: |
Speed
brakes are out. 3.5 going down hill a little bit, Bob. |
|
|
Rushworth: |
73,000
feet. |
|
|
NASA
1: |
Have
you at 4000 fps. Roger, 120 seconds now. |
|
|
Rushworth: |
Shutdown
at 122 on my watch. |
|
|
NASA
1: |
Roger,
we have it, speed brakes in please. |
|
|
Rushworth: |
Brakes
are in. |
|
|
NASA
1: |
69,000.
Put your speed brakes in, please. |
|
|
Rushworth: |
My
speed brakes are in, I'll go back up hill. |
|
|
NASA
1: |
Track
is real good. We show you about 68,000. |
|
|
Rushworth: |
68,000,
right. .......... 32° angle of attack. |
|
|
NASA
1: |
OK.
3200 velocity. Track is perfect. |
|
|
Rushworth: |
I
have RAS on and the light is still on. |
|
|
NASA
1: |
Which
light is that, Bob? |
|
|
Rushworth: |
"RAS
out" light is on. |
|
|
NASA
1: |
OK.
Show you down hill very slightly now, about 65, 66,000. Just passed over
pilot knob target. |
|
|
Rushworth: |
RAS
is off, Cuddeback. |
|
|
NASA
1: |
You're
about 8 miles out from Cuddeback, come a degree or two to the right. |
|
|
Rushworth: |
Roger.
Seems to be a little more drag here than we planned for. |
|
|
NASA
1: |
You're
a little lower in altitude now, you're 60,000 feet. |
|
|
Rushworth: |
Right. |
|
|
NASA
1: |
Just
passed over the south end of Cuddeback. 2100 fps. |
|
|
Rushworth: |
22
was what I got. Chase, you are in front of me now. |
|
|
Chase: |
Rog. |
|
|
Rushworth: |
I'm
down 2000. 1.8 on my systems. Swing a little bit to the right. Switch to
land. Engine master off. |
|
|
NASA
1: |
Speed
brakes, Bob? |
|
|
Rushworth: |
OK,
just found the lake. Going down hill and I will swing around a little bit
to the right, parallel to the highway, swing her on down again. Have 1.5,
54,000. |
|
|
NASA
1: |
OK,
we have you about 7 miles north high key. |
|
|
Rushworth: |
1.3 |
|
|
NASA
1: |
Checks. |
|
|
Rushworth: |
50,
48, 1.2 I should just about be over North Base. |
|
|
NASA
1: |
Right,
Bob, and 41,000. Show you subsonic now. |
|
|
Rushworth: |
Just
about subsonic. |
|
|
NASA
1: |
OK,
when you get a chance, camera mode switch land. |
|
|
Rushworth: |
At
land. |
|
|
Chase: |
Haven't
got you yet. |
|
|
Rushworth: |
1
mile north of NASA, NW and I'm showing 32,000 feet. |
|
|
NASA
1: |
OK,
that's pretty good here. |
|
|
Rushworth: |
Right.
Ready to go to jettison? |
|
|
NASA
1: |
Whenever
you're set, go ahead. |
|
|
Rushworth: |
Jettison.
Got anything? |
|
|
Chase: |
Rog. |
|
|
NASA
1: |
The
RAS system is disengaged, Bob? |
|
|
Rushworth: |
RAS
is off. Landing SAS is now engaged. Circuit breakers are in. |
|
|
NASA
1: |
Ok,
flap circuit breakers are in, confirm. |
|
|
Rushworth: |
Affirmative.
Lox source is down. 350, I'll slow up. |
|
|
NASA
1: |
We
have you at 20,000 feet now. How are your speed brakes? |
|
|
Rushworth: |
They're
in. |
|
|
NASA
1: |
OK.
You can pressurize tanks whenever you desire. |
|
|
Rushworth: |
Pressurize
at 17. |
|
|
NASA
1: |
OK,
take over. |
|
|
Rushworth: |
Roger. |
|
|
NASA
1: |
Show
you about 15,000 on down wind. |
|
|
Rushworth: |
I
have 14. Coming down. 10,000, flaps. |
|
|
Chase: |
Flaps. |
|
|
Rushworth: |
Gear. |
|
|
Chase: |
It's
down. It's off here. .......... beautiful |
|
|
Rushworth: |
Hyd.
pressures are OK. Temps are OK. Peroxide tank press is OK. 2400 on #l and
2600 on #2. APU bearing temps are OK. No low lights. Mixing chamber temps
are #l -25, and #2 +10. No lox source left. #l and #2 are at 1750. APU
source press is #l 2350, and #2 2550. Cabin source is 2050. 3 axis ball
heading is 172°. Inertial altitude is 11,000. Inertial climb just on
the + side. X-15 oxygen is 2000. Speed brakes are closed, SP going off,
press cooling off. |