Flight Profiles
Delta IV
Lift-off Vehicle = 0 sec | IV-M |
IV-M+ (4,2) |
IV-M+ (4,2) |
IV-M+ (5,4) |
IV-M+ (5,4) |
DSCS-III A3 | Eutelsat W5 | GPS-Navstar-III (2) | WSG-4 | WGS-8 | |
Burnout boosters |
- | + 94.1 | + 93.1/ + 93.3 | + 91.6/ + 93.1 | |
Separation boosters |
- | + 100.0 | + 100.0 | + 100.0/ +102.4 | + 100.0/ + 102.4 |
First stage thrust: 57% |
+ 221.8 | + 238.5 | ? | ? | ? |
Burnout first stage |
+ 259.9 | + 244.8 | + 235.9 | + 246.9 | + 236.0 |
Separation first stage |
+ 270.9 | + 255.8 | + 242.4 | + 254.0 | + 242.0 |
Ignition Centaur stage |
+ 284.4 | + 269.3 | + 256.9 | + 267.0 | + 255.0 |
Jettison fairing |
+ 294.5 | + 279.0 | + 266.9 | ? | ? |
Cut-off engine |
+ 853.4 | + 786.4 | + 813.1 | + 1,242.9 | + 1,191.8 |
Restart engine |
+ 1,563.0 | + 1,406.4 | + 4,007.3 | + 1,707.5 | + 1,765.6 |
Cut-off engine |
+ 1,811.2 | + 1,705.7 | + 4,214.6 | + 1,895.8 | + 1,953.6 |
Separation spacecraft |
+ 2,521.7 | + 2,255.7 | + 6,926.6 | + 2,442.0 | + 2,503.6 |
Lift-off Vehicle = 0 sec |
IV-HLV |
IV-HLV | IV-HLV | IV-HLV |
|
Demosat | GEO (DSP) | EFT-1 | Parker Solar Probe |
First stage thrust: 57% |
+ 55.0 | + 55.0 | ? | |
Burnout boosters |
+ 245.3 | + 245.3 | + 234 | |
Separation boosters |
+ 248.4 | + 248.4 | + 236 | + 237.6 |
First stage thrust: 100% |
+ 254.3 | + 254.3 | + 237 | |
Burnout first stage |
+ 333.4 | + 333.4 | + 330 | + 335.9 |
Separation first stage |
+ 341.0 | + 341.0 | + 333 | + 342.4 |
Ignition Centaur stage |
+ 354.0 | + 354.0 | + 349 | + 355.4 |
Jettison fairing |
+ 364.5 | + 364.5 | + 375 | + 365.4 |
Cut-off engine |
+ 767.8 | + 767.8 | + 1,059 | + 637.1 |
Restart engine |
+ 1,229.5 | + 4,536 | + 6,926 | + 1,345.4 |
Cut-off engine |
+ 1,711.6 | + 4,925 | + 7,209 | + 2,198.9 |
Restart engine |
+ 20,233.0 | + 22,228 | - | - |
Cut-off engine |
+ 20,427.3 | + 22,403 | - | - |
Separation Centaur stage | - | - | - | + 2,229 |
Star-48BV | - | - | - | + 2,249 ...... 2,338 |
Separation spacecraft |
+ 20,977.5 | + 22,797 | + 12,221 | + 2,598 |