Table 4.
Summary of ΔV requirements.
| From | To | ΔV (km/s) | Xfer (days) | Reference |
|---|---|---|---|---|
| LEO (407 km) | TLI | 3.276 | <1 | Mueller (2012)* |
| **TLI | Lunar Surface | 2.900 | 5 | Copernicus SW ** |
| TLI | LLO (100 km) | 0.952 | 5 | Mueller (2012)* |
| TLI | NRHO | 0.450 | 5 | DAC2 |
| NRHO | LLO (100 km) | 0.740 | <1 | DAC2 |
| LLO (100 km) | Lunar Surface | 2.180 | <1 | Mueller (2012)* |
| RPOD | Any | 0.045 | <1 | DAC2 |
| LLO 2.5° Plane Change | Lunar Surface | 0.071 | 0 | Calculated *** |
| Lunar Surface | LLO (100 km) | 1.968 | <1 | Mueller (2012)* |
| LLO (100 km) | TEI | 1.256 | <1 | Mueller (2012)* |
| LLO (100 km) | NRHO | 0.850 | <1 | DAC2 |
| NRHO | TEI | 0.450 | <1 | DAC2 |
| TEI | Splashdown | 0.011 | 5 | Mueller (2012)* |
* Includes 5% reserve.
** NASA software simulation, COPERNICUS program.
*** See Appendix B for Calculations.