Le ndatshana yabhalwa nguLocal Solar System ilungu leqembu le Foundation futhi ingathuthukiswa ngumbuyekezi oqeqeshiwe. Ingabe uqeqeshiwe kulolu daba? Sicela uhlela
Lapha imithetho ethakazelisayo yokundiza kwe-orbit: ukufinyelela phezulu uhamba kancane, futhi uhambe phezulu uhamba ngokushesha, ngemuva kwalokho uphela uhamba kancane. UWalter Hohmann, umnjiniyela waseJalimane wedolobha, wasebenza ngo-1925 indlela elula kakhulu yokuzulazula phakathi kwezinkanyezi ezimbili ezijikelezayo. Kuyinto encane kakhulu.
Ukhawulela ukunyuka, futhi ufika ngokucophelela kunalokho okwenzekile.
Bona
- Bhekisa 1, phambili. Isivinini esingeziwe asikwenza isibhakabhaka sihambe ngokushesha kakhulu ngaso lonke ikhanda: liwumisa uhlangothi lwekhanda libe yi-ellipsis. Ingxenye ephansi ihlala lapho umlilo usuvele ukhona khona; ingxenye esenyakatho ikhuphuka iye kuphakame okuzofinyelelwa kulo.
- Isiqhingi. Ingxenye ye-orbit ngaphandle kwenjini. I-satellite ikhuphuka futhi, njengebhola elithunyelwe phezulu, ihamba kancane njengoba ihamba.
- Bhala 2, uqhubekele phambili futhi. Ephezulu manje kunzima kakhulu ukuhlala khona futhi kuzobuyela emuva. Ukucindezela okulandelayo kwenza i-orbit ibe yi-circular kuphakame okutsha.
Kusuka ku-300 km kuya e-geostationary orbit, izidleke ezimbili zihlanganisa cishe 3.9 km/s, futhi indiza ithatha cishe 5 amahora 17 imizuzu.
Ukuqonda
Isivinini kunoma yisiphi isiqephu se-orbit sivela e-vis-viva: v = √(μ(2/r − 1/a)). I-Hohmann transfer ellipse ithinta izingqimba zombili, ngakho-ke umcibisholo wayo omkhulu ophakathi u_t = (r₁ + r₂)/2.
| Umzila (km) | Isivinini (km/s) | |
|---|---|---|
| Ijikeleza ku-300 km | 6,678 | 7.73 |
| Ukudluliswa, indawo ephansi | 6,678 | 10.15 |
| Ukudlulisa, indawo ephezulu | 42,164 | 1.61 |
| 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. I-coast iyingxenye yesikhathi sokuguqulwa kwe-elips: π√(a_t³/μ) ≈ amahora angu-5.3.
(Izindiza ezihamba nge-geostationary zidinga futhi ukushintsha i-orbit’s tilt kusuka esiteshini sokuqala se-latitude kuya kwe-equator, okubiza kakhulu; ukuqala eduze kwe-equator kulondoloza isithako.)
Umphathi
Δv₁ = √(μ/r₁)·(√(2r₂/(r₁+r₂)) − 1), Δv₂ = √(μ/r₂)·(1 − √(2r₁/(r₁+r₂)))
Ukulungiswa kwe-Hohmann kuyindlela encane yokulungiswa kwezingcindezi ezimbili phakathi kwama-orbit ajikelezayo, kuze kube yilapho i-r₂/r₁ < 11.94. Uma kuqhathaniswa nenani elifanayo, ukudluliswa kwe- bi-elliptic (ukulahleka okuthathu, ngaphezu ko target lokuqala) kuthatha isikhathi esincane Δv, ngentengo yesikhathi esiningi.
Ukudlidliza endaweni ephansi kuyindawo engcono kakhulu yokufaka amandla: Imiphumela emibi ithi Δv enikezwe ishintsha amandla okuhamba ngamandla lapho isithunywa sezulu sihamba ngokushesha kakhulu, ngoba Δε ≈ v·Δv.
Zama
Sebenzisa i-vis-viva ukuhlola isivinini esiphezulu sokulungiswa: μ = 398,600 km³/s², r = 42,164 km, a = 24,421 km. Ngemuva kwalokho uyilinganise nesikhathi sokujikeleza esingu-42,164 km. Ushintsho luyingozi yesithathu.
Iningi. Izinhlekelele zikhona lapho ukufunda kuqhubeka khona.
Umbuzo osheshayo
3 imibuzo esheshayo. Khetha impendulo ukuze ubone uma ulungile.
-
Ukufinyelela esigabeni esiphezulu sokugeleza, ukudlidliza okuqala ku:
- A Phezulu
- B Iya phambili, isheshisa
- C Iya emuva, ihamba kancane
- D Ngakwesobunxele, ngaphandle kweplanethi ye-orbit
Bonisa impendulo
B. Iya phambili, isheshisa
-
Ngonyaka phakathi kwezintaba ezimbili, i-satellite:
- A Ikhawulela njengoba ikhuphuka
- B Ihamba kancane uma ikhuphuka
- C Igcina isivinini esifanayo
- D I stops at the top
Bonisa impendulo
B. Ihamba kancane uma ikhuphuka Ukunyuka eduze kweplanethi kushintsha amandla kagesi abe amandla anamandla, njengebhola elithunyelwe phezulu.
-
Kungani i-geostationary orbit isetshenziswa?
- A Itholakala eduze kweplanethi
- B I-satellite ithatha usuku olulodwa nge-orbit, ngakho ihlala endaweni efanayo
- C Akukho namandla omhlaba lapha
- D I-orbit ehamba ngokushesha kakhulu
Bonisa impendulo
B. I-satellite ithatha usuku olulodwa nge-orbit, ngakho ihlala endaweni efanayo
Ingxenye yelayini
- Funda isifundo
- Ukwenze kanjani isiphakamiso
- Uthathe isifundo
Phawula isifundo siqediwe ukuze uyigcine ekwenzeni kwakho kulolu hlelo.
Isifundo siqediwe. Kulungile!
Phezulu okulandelayo Qala amafasitela: indlela eya eMarsAmagama kule ncwadi
Amasu
- 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
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