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Guhindura... in Umuvuduko Kuri Himura hagati,, i, na i.

ESO/S. Guisard (www.eso.org/~sguisard) (CC BY 4.0)

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ni? A Bya Umwanya. Umurongo: ni Rimwe Bya A, na Umubare A Guhindura... Umuvuduko Kuri. Hejuru i na Kubona i Umwanya.

Gukoresha: A Tangira & vendorShortName; na A Intego: Kabiri Utudomo ku i, Koresha i na Ibikubiyemo, Cyangwa Kanda Rimwe Bya i Utubuto. Hejuru na i Umurongo: & Ongera Hejuru.

Gushakisha

kugirango iyi

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    i A A A: A Inzira Umurongo: A - Agaciro Two numbers, like 9.4 / 0: the cost going one way and the cost coming back. Coming back can be cheaper when air does the braking.

    Guhindura... in Umuvuduko Kuri Himura hagati,, i, na i. 9,4 / 0 2,45 1,48 3,22 3,13 0,82 1,63 3,61 2,09 0 / 4,1 4,11 9,48 Ubuso Low Earth orbit(200 km) Guhinduraizina... Ishusho Gusohoka Kuri i (100 km) Ukwezi Kuri Low Mars orbit(300 km) Ubuso - Asteroide Ishusho

    Kuri i

    Uduciro -, Ibimenyetso. & Ongera na Igishushanyo Amahinduka.

    iyi
    1. Kuri Gyayo Kuva: Ubuso Kuri GitoyaIcyegeranyo: That first step costs 9.4 km/s. Going on from orbit all the way to the Moon's surface costs only about 5.6 km/s more.
    2. i Hanyuma na Gutandukanya i.Icyegeranyo: They are almost the same: about 15.0 and 15.1 km/s, even though Mars is always more than a hundred times farther away than the Moon. Mars has air to brake with when you land; the Moon has none, so every bit of slowing down costs fuel.
    3. A Kuva: Umurongo: Inyuma Kuri Umurongo:.Icyegeranyo: The last leg, down to Earth's surface, costs 0 km/s: Earth's air and a heat shield do the braking, as they did for every Apollo crew. Climbing off Mars still costs about 4.1 km/s.
    4. "Na: Kuva: Hasi Kuri Hasi.Icyegeranyo: Reaching the high orbit where TV and weather satellites sit costs about the same as reaching orbit around the Moon: about 3.9 km/s from low Earth orbit in both cases.
    Kuri
    Ibitekerezo

    ni - V?

    Bya A. Hejuru Igihe Umuvuduko Hejuru na buri Igihe: Igiteranyo ni Delta - V. Umwanya ni Oya Kuri Guca na Oya, buri Amahinduka Bya Umuvuduko, Hejuru Cyangwa Hasi, Kuri Kuva: i Urufaya, na buri Bya.

    ni Kuri i Intera?

    Being in orbit is not about being high up. It is about going sideways so fast that you keep falling around Earth instead of into it. Just above the air that means about 7.8 km/s (about 28,000 km/h), once round the planet in about 90 minutes. On the way up a rocket also loses roughly 1.5 to 2 km/s fighting gravity and air drag (Earth's spin gives a little back), so this one step costs about 9.4 km/s.

    ni ku ku i?

    Mars has a thin atmosphere. A lander hits that air at high speed and its heat shield turns the speed into heat; parachutes and a short rocket burn at the end do the rest. So the map counts 0 km/s of rocket fuel for landing on Mars, but 1.63 km/s for the airless Moon, where engines must do all the braking. Leaving Mars is another story: climbing back up to orbit costs about 4.1 km/s.

    ni?

    Using a planet's air as a free brake. A spacecraft dips into the thin top of the atmosphere, drag slows it, and it saves fuel it would otherwise burn. In 2006 NASA's Mars Reconnaissance Orbiter shrank its orbit this way, with hundreds of dips through Mars's upper air over about five months.

    km S?

    A rocket has to carry its own fuel, and that fuel has to be pushed along too. So each extra km/s needs more fuel than the one before. That is why the Saturn V that sent astronauts to the Moon weighed nearly 3,000 tonnes at launch, most of it propellant.

    123
    : i i Hejuru: Bya i ku, na.

    : Koresha Bisanzwe Kabiri - Inzira Na: NASA/ Ibyatanzwe (Inyandikoporogaramu -); Kuva: i - V Ingingo ku na Indango. Gutangiza: NASA.: NASA/JPL

    Ibyatanzwe imbonerahamwe# Umwandiko Igisubizo
    Amahuza ku i
    BivuyeKuri→←Byakoreshejwe
    UbusoLow Earth orbit (200 km) 9,4 km/s 0 km/s (Koresha) (): 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)Guhindura izina... 2,45 km/s 2,45 km/s (Koresha) (): Hohmann perigee burn, 200 km to 35,786 km altitude, equatorial
    Guhindura izina...Ishusho 1,48 km/s 1,48 km/s (): Hohmann apogee burn, no plane changeA Tangira & vendorShortName; Ipaji: Kuva: i, Guhindura... i OYA Kyongewe A Isigamwanya.
    Low Earth orbit (200 km)Gusohoka 3,22 km/s 3,22 km/s (Koresha) (): Escape speed minus circular speed at 200 km
    Low Earth orbit (200 km)Kuri i 3,13 km/s 3,13 km/s (Koresha) (): Raise apogee to the Moon's mean distance
    Kuri i(100 km) 0,82 km/s 0,82 km/s (): Patched conic capture into a 100 km lunar orbit
    (100 km)Ukwezi 1,63 km/s 1,63 km/s (): Circular speed at 100 km (ideal, no gravity losses; real landings need more)
    Low Earth orbit (200 km)Kuri 3,61 km/s 3,61 km/s (Koresha) (): Earth-Mars Hohmann departure from 200 km, Oberth effect included
    KuriLow Mars orbit (300 km) 2,09 km/s (Koresha) 2,09 km/s (): Capture into a 300 km circular Mars orbit
    Low Mars orbit (300 km)Ubuso 0 km/s (Koresha) 4,1 km/s (): Delta-v budget (Wikipedia, with its cited references), typical values including lossesi (Ikirere na); i Inyuma Kuri ni i Agaciro:.
    Low Earth orbit (200 km)- Asteroide 4,11 km/s 4,11 km/s (Koresha) (): 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)Ishusho 9,48 km/s 9,48 km/s (Koresha) (): 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

    na Koresha ya:. OYA Byakoreshejwe ya: Ibuganya, Cyangwa Icyo ari cyo cyose. Kigenga na -. i Ibigize