Delta-v Map
Olee mgbanwe n'ụdị ọsọ ọ ga-ewe iji kpụga n'etiti ụwa, orbit, ọnwa, Mars na asteroids.
ESO/S. Guisard (www.eso.org/~sguisard) (CC BY 4.0)
Delta-v Map
Delta-v zuru ezu
Nzọụkwụ
Valiu bụ ụzọ otu, n'ihi na ọbụla akọwapụtara ya dị ka nke dị iche. Ọrụ eziokwu na-agbakwunye mmebi na mgbanwe plane.
Táàbụ̀ data (nhọrọ ngwe)
| Site na | Ka | → | ← | Otú ọ dị ejiri ya rụọ ọrụ |
|---|---|---|---|---|
| Usoro ala | Òbì ala ụwa (200 km) | 9.4 km/s | 0 km/s (nwere ike iji aerobraking) | Tíìpìì (e bipụtara): Delta-v budget (Wikipedia, with its cited references), typical values including lossesN'okporo ụzọ: ihe dịka 7.8 km/s nke ọsọ okporo ụzọ nakwa nkwụsịtụ maka mgbagha na ikuku. |
| Òbì ala ụwa (200 km) | Geostationary transfer orbit | 2.45 km/s | 2.45 km/s (nwere ike iji aerobraking) | E hiwere (ọdịnaya): Hohmann perigee burn, 200 km to 35,786 km altitude, equatorial |
| Geostationary transfer orbit | Geostationary orbit | 1.48 km/s | 1.48 km/s | E hiwere (ọdịnaya): Hohmann apogee burn, no plane changeSite n'ebe a na-ebubata ya n'ebe dị anya site n'equator, ịgbanwekwa orbit nke tilt na-agbakwunye ọtụtụ puku mita kwa sekọnd. |
| Òbì ala ụwa (200 km) | Escape Earth | 3.22 km/s | 3.22 km/s (nwere ike iji aerobraking) | E hiwere (ọdịnaya): Escape speed minus circular speed at 200 km |
| Òbì ala ụwa (200 km) | Kpụga na Mọnde | 3.13 km/s | 3.13 km/s (nwere ike iji aerobraking) | E hiwere (ọdịnaya): Raise apogee to the Moon's mean distance |
| Kpụga na Mọnde | Óbìtị̀ ala nke ọnwa (100 km) | 0.82 km/s | 0.82 km/s | E hiwere (ọdịnaya): Patched conic capture into a 100 km lunar orbit |
| Óbìtị̀ ala nke ọnwa (100 km) | Mkpụrụedemede | 1.63 km/s | 1.63 km/s | E hiwere (ọdịnaya): Circular speed at 100 km (ideal, no gravity losses; real landings need more) |
| Òbì ala ụwa (200 km) | Kpụga na Mars | 3.61 km/s | 3.61 km/s (nwere ike iji aerobraking) | E hiwere (ọdịnaya): Earth-Mars Hohmann departure from 200 km, Oberth effect included |
| Kpụga na Mars | Óbìtị̀ ala Mars (300 km) | 2.09 km/s (nwere ike iji aerobraking) | 2.09 km/s | E hiwere (ọdịnaya): Capture into a 300 km circular Mars orbit |
| Óbìtị̀ ala Mars (300 km) | Oge | 0 km/s (nwere ike iji aerobraking) | 4.1 km/s | Tíìpìì (e bipụtara): Delta-v budget (Wikipedia, with its cited references), typical values including lossesN'ịla elu, a na-eji ikuku (ihe ọkụ na parachutes) arụ ọrụ; ịgagharị n'okporo ụzọ bụ uru dị ka ọ dị. |
| Òbì ala ụwa (200 km) | N'okpuru-Earth asteroid (Bennu) | 4.11 km/s | 4.11 km/s (nwere ike iji aerobraking) | E hiwere (ọdịnaya): Heliocentric Hohmann 1 au to Bennu's semi-major axis, coplanar (ignores its 6 degree inclination and its eccentricity); departure from 200 km LEO |
| Òbì ala ụwa (200 km) | Ceres orbit | 9.48 km/s | 9.48 km/s (nwere ike iji aerobraking) | E hiwere (ọdịnaya): Heliocentric Hohmann 1 au to Ceres, coplanar (ignores its 10.6 degree inclination); departure from 200 km LEO, capture into a 200 km Ceres orbit |
Ngwaọrụ na agụụ na-eji móòdù akọwapụtara maka ịmụ naanị. Ha gaghị eji ha maka nlegharị anya, mmepe ọrụ mọọbụ nhọrọ ọbụla nke ọrụ. Saịtịapụl bụ n'efu ma ọ bụghị n'aka. Gụọ n'ihe ọmụmụ ihe ndị ahụ