ESO/S. Guisard (www.eso.org/~sguisard) (CC BY 4.0)
Delta-v Map
Delta-v Jumma'a
Mataki
Kima ne na hanya daya, dabarun gudu masu kyau sai dai idan an nuna su a matsayin na musamman. Aikin gaskiya yana ƙara asarar da canji na jirgin sama.
Jadawalin bayanai (zaɓin rubutu)
| Daga | @ action | → | ← | Yãya aka yi shi? |
|---|---|---|---|---|
| QFontDatabase | Low Earth orbit (200 km) | 9.4 km/s | 0 km/s (QShortcut) | @ action: Delta-v budget (Wikipedia, with its cited references), typical values including lossesLaunch to orbit: about 7.8 km/s of orbital speed plus losses to gravity and air drag. |
| Low Earth orbit (200 km) | Geostationary transfer orbit | 2.45 km/s | 2.45 km/s (QShortcut) | dakata: Hohmann perigee burn, 200 km to 35,786 km altitude, equatorial |
| Geostationary transfer orbit | Geostationary orbit | 1.48 km/s | 1.48 km/s | dakata: Hohmann apogee burn, no plane changeDaga wurin da aka fara daga arewa maso gabas, kuma canja tsayin orbit na ƙara ɗaruruwan mita a kowace sakan. |
| Low Earth orbit (200 km) | Earth escape | 3.22 km/s | 3.22 km/s (QShortcut) | dakata: Escape speed minus circular speed at 200 km |
| Low Earth orbit (200 km) | QDialogButtonBox | 3.13 km/s | 3.13 km/s (QShortcut) | dakata: Raise apogee to the Moon's mean distance |
| QDialogButtonBox | Low lunar orbit (100 km) | 0.82 km/s | 0.82 km/s | dakata: Patched conic capture into a 100 km lunar orbit |
| Low lunar orbit (100 km) | Moon surface | 1.63 km/s | 1.63 km/s | dakata: Circular speed at 100 km (ideal, no gravity losses; real landings need more) |
| Low Earth orbit (200 km) | QDialogButtonBox | 3.61 km/s | 3.61 km/s (QShortcut) | dakata: Earth-Mars Hohmann departure from 200 km, Oberth effect included |
| QDialogButtonBox | Mars orbit low (300 km) | 2.09 km/s (QShortcut) | 2.09 km/s | dakata: Capture into a 300 km circular Mars orbit |
| Mars orbit low (300 km) | Mars surface | 0 km/s (QShortcut) | 4.1 km/s | @ action: Delta-v budget (Wikipedia, with its cited references), typical values including lossesA cikin wannan yanayin, za a iya amfani da shi don yin amfani da tsarin aiki na farko (wanda aka sani da "Alpha"). |
| Low Earth orbit (200 km) | star name | 4.11 km/s | 4.11 km/s (QShortcut) | dakata: Heliocentric Hohmann 1 au to Bennu's semi-major axis, coplanar (ignores its 6 degree inclination and its eccentricity); departure from 200 km LEO |
| Low Earth orbit (200 km) | star name | 9.48 km/s | 9.48 km/s (QShortcut) | dakata: 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 |
@ info: status Ka karanta bayanin da ke cikin shirin koyarwa