Le ncwadi yabhalwa ngu Local Solar System Iqela le-Fundamente lilungu kwaye lingaphuculwa ngumvavanyi oqeqeshiweyo. Ingaba uqeqeshiwe kulo mxholo?
Apha kukho imithetho enomdla kakhulu yokuhamba ngenqwelo-moya: ukutsala ukhawuleze, kwaye ukuba uhambe phezulu ukhawuleze, emva koko uphele uhambe phantsi. UWalter Hohmann, umyili waseJamani wedolophu, wasebenza ngo1925 indlela ekhawulezayo yokuqhuba phakathi kweendawo ezimbini ezijikelezayo. Imalunga nesatellite nganye ekwi orbit yendawo ehlala kuyo i-geostationary yafika apho isebenzisa le mbono.
Yiya phezulu ukunyuka, kwaye ufike ngokucothayo kunokuba washiya.
Bona
- Gcina 1, phambili. Isantya esithe nkqo asiyi kwenza i-satellite ihambe ngokukhawuleza ngaphezulu kojikelezo lwayo: iphakamisa ujikelezo lube yi elipsis. Inqanaba eliphantsi lihlala apho ukutshisa kwenzeke khona; icala elincinane linyuka ukuya kwinqanaba elifanelekileyo lobude.
- Ilwandle. Ingxenye ye orbit ngaphandle kwenjini. I-satellite inyuka kwaye, njengebhola eqhutywa phezulu, ihamba ngokucothayo njengoko ihamba.
- Gcina 2, iqhubekeka phambili kwakhona. Kwisiphelo sendlela ngoku iyacotha kakhulu ukuba ihlale apho kwaye izakubuyela umva. Uxinzelelo lwesibini lusenza i-orbit ijikeleze kwinqanaba elitsha lobude.
From 300 km to geostationary orbit the two burns add up to about 3.9 km/s, and the trip takes about 5 hours 17 minutes.
Ukuqonda
Isantya kwindawo naliphi na le orbit ivela kwi-vis-viva: v = √ (μ(2/r − 1/a)). I-Hohmann transfer ellipse iqhatha zonke izijikelezi, ngoko ke umgca wayo ophakathi mkhulu yi a_t = (r₁ + r₂)/2.
| Umda (km) | Isantya (km/ s) | |
|---|---|---|
| Ijikeleza kwi 300 km | 6,678 | 7.73 |
| Unikezelo, incopho ephantsi | 6,678 | 10.15 |
| Unikezelo, incopho ephezulu | 42,164 | 1.61 |
| Ijikelezayo, i-geostationary | 42,164 | 3.07 |
Umlilo 1 = 10.15 − 7.73 ≈ 2.43 km/s. Umlilo 2 = 3.07 − 1.61 ≈ 1.47 km/s. Ilwandle liphesenti yexesha lokudlulisela i-ellipsis: π√(a_t³/μ) ≈ iiyure ezili-5.3.
(Izithuthi ezihlala zijikeleza ihlabathi kufuneka zitshintshe ubukhulu bendawo ejikelezayo ukusuka kwilayini ye latitude ukuya kwi-equator, oku kuthatha ixesha elide; ukuthutha kufutshane ne-equator kukhusela ifuthe.)
Umphathi
Δv₁ = √(μ/r₁)·(√(2r₂/(r₁+r₂)) − 1), Δv₂ = √(μ/r₂)·(1 − √(2r₁/(r₁+r₂)))
Uthutho lweHohmann luyimfuneko yothutho olunoxinzelelo olubini phakathi kweendawo ezijikelezayo zeplanethi, kude kube r₂/r₁ < 11.94. Ngapha koko uthelekiso bi-elliptic lokudlulisa (ukutshisa okuthathu, ukudlula kwinjongo yokuqala) iindleko ezincinci Δv, ngexabiso lexesha elininzi.
Ukutshisa kwindawo ephantsi kulapho kusebenza khona kakuhle ukudibanisa amandla: i-Oberth effect ithetha ukuba u-Δv onikezelwe utshintsha amandla okujikeleza kakhulu apho inqanawa yendawo yokuhamba ngokukhawuleza, kuba Δ ≈ v·Δv.
Zama
Sebenzisa i-vis-viva ukujonga isixa esiphezulu sokuhambisa: μ = 398,600 km³/s², r = 42,164 km, a = 24,421 km. Emva koko uyithelekise nesantya esijikelezayo kwi 42,164 km. Utshintsho luyingozi yesibini.
Iingxaki zikhona apho ukufunda kuqhekeka khona.
Uvavanyo olukhawulezayo
3 imibuzo ekhawulezayo. Khetha impendulo ukuze ubone ukuba ulungile na.
-
Ukufikelela kwi-orbit ejikelezayo ephezulu, ukutshisa kuqala ku:
- A Phezulu
- B Ihamba phambili, ikhawulezisa
- C Ukuhamba umva, ukucotha
- D I-Orbit
Bonisa impendulo
B. Ihamba phambili, ikhawulezisa
-
Ngexesha lolwandle phakathi komlilo ombini, i-satellite:
- A Ikhawuleza njengoko inyuka
- B Icotha xa inyuka
- C Igcina isantya esifanayo
- D I stops at the top
Bonisa impendulo
B. Icotha xa inyuka Ukunyuka phezulu ukusuka ehlabathini kutshintshiselana nge-kinetic energy ye-potential energy, njengebhola eqhutywa phezulu.
-
Kutheni i-geostationary orbit isetyenziswa?
- A Iiplanethi
- B Isiqhagamshelanisi selanga sithatha ubusuku obunye kwi-orbit, ngoko sihlala ngaphezulu kwendawo efanayo
- C Akukho mthwalo wengqondo apho
- D I-orbit ekhawulezayo
Bonisa impendulo
B. Isiqhagamshelanisi selanga sithatha ubusuku obunye kwi-orbit, ngoko sihlala ngaphezulu kwendawo efanayo
Iilayini Ezigqibekileyo
- Funda isifundo
- Ukwenza isigqibo
- Uthathe isifundo
Phawula isifundo sencwadi eneenkcukacha egqityiweyo ukusigcina kwindlela yakho yokuqhubekeka kule sixhobo.
Isifundo sigqityiwe. Yenziwe kakuhle!
Phezulu Okulandelayo Launch Windows: the road to MarsNameAmagama kule ncwadi eneenkcukacha
IiNkqubo
- 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
Eli nqaku lilayisensiwe CC BY-SA 4.0.