| Booster |
5.5-segment SRB derived from Shuttle |
| Core |
6 RS-68 engines/33ft diameter Al-Li tank |
| EDS |
1 J-2X Engine/33ft diameter Al-Li tank |
| Orbit |
130 nmi circular at 29 deg |
| Gross Injected Mass to LEO |
413,888 lbm |
| Payload to TLI from 100 nmi |
156,652 lbm (includes CEV and LSAM) |
| Payload Envelope |
25.3ft x 30.0ft (length x diameter) |
| Ares V DRM Details |
- At Ignition
- Time (sec): 0.0
- Weight (lbm): 8,167,072
|
- Core Staging/EDS Ignition
- Time (sec): 303.1
- Altitude (ft): 412,277
- Mach: 11.74
|
- Maximum Dynamic Pressure
- Time (sec): 78.3
- Altitude (ft): 47,175
- Mach: 1.82
- Dynamic Pressure (psf): 680
|
- Shroud Jettison
- Time (sec): 308.3
- Altitude (ft): 414,986
- Mach: 10.91
|
- SRB Separation
- Time (sec): 121.6
- Altitude (ft): 120,664
- Mach: 4.24
|
- EDS MECO
- Time (sec): 774.3
- Altitude (ft): 800,057
- Orbit: 130 nmi at 29.0 deg
|
