[Main]
Info=Saturn V Launch Vehicle Flight Evaluation Report AS-506 Apollo 11 Mission (September 20, 1969)
http://ru.scribd.com/doc/47696632/Saturn-V-Launch-Vehicle-Flight-Evaluation-Report-AS-506-Apollo-11-Mission
Timeline: http://history.nasa.gov/SP-4029/Apollo_11i_Timeline.htm
Table 20-1
- Holddown Arm Relfase (Act) Time .30sec
Total Vehicle 2,899,008 kg (0.3 sec)
- Tower clearance yaw maneuver started 1.7 sec
- Yaw maneuver ended 9.7 sec
- Pitch and roll maneuver started 13.2 sec
- Roll maneuver ended 31.1 sec
- Mach 1 achieved 66.3 sec
- S-IC center engine cutoff command 135.2 sec
- Pitch maneuver ended 160.0 sec
- S-IC outboard engine cutoff 161.63 sec
Total S-IC stage 2,239,381 kg (0.3 sec)
S-IC IS small 614 kg (162.3 sec ?)
Total S-IC stage 164,381 kg (162.3 sec)
S-IC IS 5206 kg (0.0 sec), 5173 kg (162.3 sec)
S-IC IS prop 610 kg (start), 309 kg (164.0 sec), 0.0 kg (166.20 sec)
- S-IC/S-II Separation (Act) time 162.3 sec
x---x---x---x---x---x---x---x---x---x---x
Total S-II stage 479,964 kg (start), 479,706 kg (162.3 sec; 164.0 sec), 479,112 kg (166.2 sec)
- S-II ignition 164.0 sec
- S-II aft interstage jettisoned 192.3 sec
S-IC IS large 3982 kg
- Launch escape tower jettisoned 197.9 sec
- S-II center engine cutoff 460.62 sec
- S-IC impact 543.7 sec
- S-II outboard engine cutoff 548.22 sec
Total S-II stage 43,436 kg (549 sec)
Total S-II/S-IV IS 3663 kg (550 sec ?)
x---x---x---x
Total Vehicle 166,571 kg (552.2 sec)
Total S-IVB stage 118,939 kg (552.2)
- S-IVB 1st burn ignition 552.20 sec
- S-IVB ullage case jettisoned 561.0 sec
- S-IVB 1st burn cutoff 699.3 sec
Total vehicle 135,182 kg (699.34 sec)
Total S-IVB stage 87,550 kg (699,34)
Total Spacecraft + InstrUnit 45,693 + 1939 = 47,632 kg (ΟΝ)
- Earth orbit insertion 709.33 sec
F-1
Thrust: 7,740.50 kN (1,740,134 lbf).
Specific impulse: 304 s.
Specific impulse sea level: 265 s.
Burn time: 161 s.
J-2
Thrust: 1,033.10 kN (232,250 lbf).
Specific impulse: 421 s.
Specific impulse sea level: 200 s.
Burn time: 475 s.
M0=2899,008
DopMass=S-IC/S-II interstage small+prop 1224 162,3
Second stage slim 852 166,2
S-IC/S-II interstage large 3982 192,3
Total Launch Escape System 4041,5 197.9
S-II/S-IVB interstage 3663 550
dTime1=0,1
itCnt1=63000
itCnt2=20000
Sh=28,4667
Dlg=-80,5585
HStart=0,1
Rpl=6378,14
Rpl2=6378,14
Mpl=5,9736E24
Vpl=460
M1r1=164,381
M1t1=2239,381
I1m1=2597
I1v1=2982
Ft1m1=34200
Ft1v1=40000
Dr1=10,1
Ton1=0
Toff1=161,63
BlocksCnt1=0
Stupen2=1
M1r2=43,436
M1t2=479,964
I1m2=1960
I1v2=4140
Ft1m2=4450
Ft1v2=5150
Dr2=10,1
Ton2=164
Toff2=548,22
StartStup2=1
BlocksCnt2=0
Stupen3=1
M1r3=87,55
M1t3=118,939
I1m3=1960
I1v3=4200
Ft1m3=890
Ft1v3=900
Dr3=6,61
Ton3=552,2
Toff3=699,33
StartStup3=2
BlocksCnt3=0
Stupen4=0
[Driving]
LinesCount=16
HighU1=1,7
AlfaU1=60
MaxmU1=18
AxisU1=1
HighU2=9,7
AlfaU2=0
MaxmU2=18
AxisU2=1
HighU3=0
AlfaU3=1
MaxmU3=89
AxisU3=0
HighU4=12
AlfaU4=10
MaxmU4=86
AxisU4=0
HighU5=25
AlfaU5=34
MaxmU5=40
AxisU5=0
HighU6=100
AlfaU6=22
MaxmU6=23,1
AxisU6=0
HighU7=164
AlfaU7=1,5
MaxmU7=0
AxisU7=0
HighU8=200
AlfaU8=-35
MaxmU8=0
AxisU8=0
HighU9=211,5
AlfaU9=6,4
MaxmU9=0
AxisU9=0
HighU10=460
AlfaU10=-26
MaxmU10=0
AxisU10=0
HighU11=467
AlfaU11=11
MaxmU11=0
AxisU11=0
HighU12=490
AlfaU12=7
MaxmU12=0
AxisU12=0
HighU13=550
AlfaU13=0
MaxmU13=0
AxisU13=0
HighU14=551
AlfaU14=17
MaxmU14=0
AxisU14=0
HighU15=560
AlfaU15=7,5
MaxmU15=0
AxisU15=0
HighU16=675
AlfaU16=60
MaxmU16=0
AxisU16=0
StartTang0=90
StartV0=0
[Aerodynamics]
LinesCount=20
Mx1=0
Cx1=0,145
Mx2=0,5
Cx2=0,15
Mx3=0,75
Cx3=0,16
Mx4=0,8
Cx4=0,2
Mx5=1
Cx5=0,38
Mx6=1,15
Cx6=0,53
Mx7=1,25
Cx7=0,56
Mx8=1,3
Cx8=0,54
Mx9=1,5
Cx9=0,51
Mx10=2
Cx10=0,43
Mx11=2,5
Cx11=0,38
Mx12=3
Cx12=0,36
Mx13=3,5
Cx13=0,34
Mx14=4
Cx14=0,3
Mx15=4,5
Cx15=0,25
Mx16=5
Cx16=0,23
Mx17=5,5
Cx17=0,21
Mx18=6
Cx18=0,19
Mx19=7
Cx19=0,16
Mx20=8
Cx20=0,14
[Throttle]
LinesCount=12
Tdr1=0
PrT1=100
Tdr2=135
PrT2=100
Tdr3=135,1
PrT3=80
Tdr4=140
PrT4=79,5
Tdr5=161,63
PrT5=80
Tdr6=164
PrT6=100
Tdr7=460
PrT7=99,9
Tdr8=460,5
PrT8=80
Tdr9=500
PrT9=80
Tdr10=500,1
PrT10=60
Tdr11=550
PrT11=59
Tdr12=552,2
PrT12=100