1
00:00:07,829 --> 00:00:04,630
vms go for launch

2
00:00:12,629 --> 00:00:07,839
copy that vm check step 101

3
00:00:14,950 --> 00:00:14,150
t minus 5

4
00:00:15,990 --> 00:00:14,960
4

5
00:00:16,950 --> 00:00:16,000
three

6
00:00:17,830 --> 00:00:16,960
two

7
00:00:46,150 --> 00:00:17,840
one

8
00:00:49,190 --> 00:00:46,160
zero zero copy that sir feel the

9
00:00:54,389 --> 00:00:49,200
avionics and boost the power numb

10
00:00:58,150 --> 00:00:55,910
the minotaur one launch vehicle is

11
00:01:00,229 --> 00:00:58,160
entering predicted max q is three miles

12
00:01:01,750 --> 00:01:00,239
downrange altitude of six miles

13
00:01:07,190 --> 00:01:01,760
traveling at a speed of sixteen hundred

14
00:01:11,270 --> 00:01:09,670
vehicle attitude and flight pattern

15
00:01:13,350 --> 00:01:11,280
we're approaching stage one separation

16
00:01:21,590 --> 00:01:13,360
stage two ignition event would occur

17
00:01:25,109 --> 00:01:23,910
we have stage one preparation and days

18
00:01:27,190 --> 00:01:25,119
with this

19
00:01:29,190 --> 00:01:27,200
phase two motor pressure is within

20
00:01:30,950 --> 00:01:29,200
prediction

21
00:01:34,870 --> 00:01:30,960
stage two rcu

22
00:01:36,710 --> 00:01:34,880
the li tvc pressures are nominal

23
00:01:42,950 --> 00:01:36,720
stage two attitude and flight path are

24
00:01:58,789 --> 00:01:44,710
field avionics and boost the power

25
00:02:06,709 --> 00:02:00,310
vehicle attitude and flight path are

26
00:02:11,430 --> 00:02:09,350
the next expected event is stage 3 tvc

27
00:02:13,910 --> 00:02:11,440
battery activation followed by the stage

28
00:02:30,710 --> 00:02:13,920
2 separation and stage 3 ignition in

29
00:02:35,589 --> 00:02:32,550
phase three pvc battery activation

30
00:02:37,990 --> 00:02:35,599
battery power looks good

31
00:02:39,830 --> 00:02:38,000
we have confirmed stage two separation

32
00:02:41,430 --> 00:02:39,840
and stage three ignition stage three

33
00:02:43,190 --> 00:02:41,440
motor pressure is expected barren

34
00:02:44,790 --> 00:02:43,200
separation will occur in approximately

35
00:02:46,550 --> 00:02:44,800
eight seconds

36
00:02:48,470 --> 00:02:46,560
stage three attitude and flight path are

37
00:02:50,390 --> 00:02:48,480
as expected

38
00:02:56,949 --> 00:02:50,400
we have confirmed staring separation

39
00:03:01,750 --> 00:02:59,670
approximately 25 seconds into the 75

40
00:03:03,110 --> 00:03:01,760
second stage 3 burn thrust vector

41
00:03:14,710 --> 00:03:03,120
actuator responses are within

42
00:03:19,830 --> 00:03:16,710
orbital guidance initiated vehicle

43
00:03:34,550 --> 00:03:19,840
attitude and performance are nominal

44
00:03:38,470 --> 00:03:36,470
we are now entering stage three mode to