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Heano muenzaniso wechirevo chinokosha chekufamba mumigwagwa: kuti uwane mukana unoramba uchinonoka, uye kuti uende kumusoro unoenderera mberi, mushure meizvozvo unotanga kunonoka. Walter Hohmann, muEngineer weguta reGermany, akawana mu1925 nzira yakachipa yekufambisa pakati pezviviri zvemaorbit. Anenge ese ma satellites ari mugeostationary orbit akasvika pano achishandisa chirongwa chake.
Kukurumidza kusvika kukwira, uye iwe unosvika zvakaoma kupfuura wakanga wakasiya.
Ona
- Burn 1, forwards. Iyo yakakura kupfuura iyo yekutanga simba haiite kuti saiti iende nekukurumidza pamusoro pechiso chake: inosimudza chiso kuita ellipse. Iyo yakaderera nzvimbo inogara panzvimbo iyo burn yakaitwa; iyo yakadzika-pasi inobva yakwira kusvika pakusvika kwechinangwa.
- Kubva panzvimbo. Half an orbit without engine. Satellite inokwira uye, sebhola rakasviba, inononoka sezvairi kuenda.
- Burn 2, forwards again. Pamusoro pechidzitiro ichi, zvino iri nyore kugara pano uye ichadzokera kumashure. A yekutanga kumanikidza inoita orbit circular patsva hurefu.
Kubva pa300 km kusvika kugeostationary orbit, zviviri izvi zvinowedzera kusvika pamamiriyoni mashanu emadhora. 3.9 km/s, uye chitima chinotora pamusoro 5 hours 17 minutes.
_Zvinyorwa
Kufamba kwechiedza kunogona kutaurwa sezvimiro zvemasimba emagetsi: v = √(μ(2/r − 1/a)). Hohmann transfer ellipse inobatawo macircles maviri, saka iyo semi-makuru axis i a_t = (r₁ + r₂)/2.
| Radius (km) | Speed (km/s) | |
|---|---|---|
| Circular pa 300 km | 6,678 | 7.73 |
| Kutumira, pasi penzvimbo | 6,678 | 10.15 |
| Kutumira, yakakwira point | 42,164 | 1.61 |
| Geostationary | 42,164 | 3.07 |
Burn 1 = 10.15 − 7.73 ≈ 2.43 km/s. Kupisa 2 = 3.07 − 1.61 ≈ 1.47 km/s. The coast is half the transfer ellipse’s period: π√(a_t³/μ) ≈ 5.3 hours.
(Zvinoitika kuti ma satellite anotanga kutenderera panyika achibva panzvimbo yekutanga anofanirawo kusarudza nzvimbo yekutanga, izvo zvinoda mari yakawanda.
Munyori
Δv₁ = √(μ/r₁)·(√(2r₂/(r₁+r₂)) − 1), Δv₂ = √(μ/r₂)·(1 − √(2r₁/(r₁+r₂)))
Hohmann kushandura ndeimwe yezvishoma zviviri-impulse kushandura pakati pe coplanar circular orbits, sezvar₂/r₁ < 11.94. Pashure peiyo ratio a bi-elliptic kushandura (matanhatu burns, kuenda kunze kwetarget yekutanga) inodhura zvishoma Δv, pamitengo yenguva yakawanda.
Kupisa panzvimbo yakaderera ndiyo nzvimbo ine simba kwazvo yekuwedzera simba: Oberth effect inoti Δv inochinja zvakanyanya orbital energy apo chikepe chepasi chiri kufamba nekukurumidza, nekuti Δε ≈ v·Δv.
Tarisa
Usashandisa vis-viva kuti uone kukwira kwesimba pakutanga kwekuchinja: μ = 398,600 km³/s², r = 42,164 km, a = 24,421 km. Saka uzvienzanisa nekumhanya kwechiedza pa42,164 km. Chimwe chinhu chinonzi iyo yekupedzisira burn.
Great. Zvipingamupinyi ndezvekuti kudzidza kunoramba kuripo.
Chidzidzo chekukurukura
3 nhanho mibvunzo. Choose mashoko kuti uone kana iwe uri zvakanaka.
-
Kuti uwane yakakwira yechinyakare orbit, yekutanga burn ndeye:
- A Kumusoro
- B Kuenda mberi, kukwira
- C Kudzoka, kunonoka
- D Pamusoro, kunze kwe orbit plane
Kuratidza mhinduro
B. Kuenda mberi, kukwira
-
Panguva yekumaodzanyemba pakati pezviviri zvinopisa, satellite:
- A Inokurumidza kupfuura sezvainokwira
- B Inononoka sezvainokwira
- C Inochengeta iyo imwecheteyo speed
- D Kudzima
Kuratidza mhinduro
B. Inononoka sezvainokwira Kukwira kubva panyika kunochinja kinetic energy kuita potential energy, sekunge bhandi rakasviba.
-
Nei geostationary orbit iri yakakosha?
- A Iyo iri pedyo nenyika
- B A satellite there takes one day per orbit, so it stays over the same spot
- C Hapana gravity pano
- D Iyo ndiyo yakanyanya kuomarara orbit
Kuratidza mhinduro
B. A satellite there takes one day per orbit, so it stays over the same spot
Kusvika pakupera
- Ona dzidziso
- Akakunda chipingamupinyi
- Akatora chidzidzo
. Kuchengeta kuenderera mberi kwebasa pane iyi kifaa, tinya paKunyora.
Chidzidzo chakapera. Yakanaka!
Kumusoro Kutanga windows: nzira kuMarsMashoko mubhuku rino
Zvinyorwa
- W. Hohmann, Die Erreichbarkeit der Himmelskörper (1925), NASA technical translation F-44
- NASA JPL, Basics of Space Flight, Chapter 4: Trajectories
- JPL SSD, Astrodynamic parameters
- R. Bate, D. Mueller, J. White, Fundamentals of Astrodynamics (Dover, 1971), ch. 3
Iyi dzidzo ine mubhadharo CC BY-SA 4.0.