ku A Local Solar System Itsinda Umunyamuryango na ku A. in iyi Ikintu?
In December 1965 Gemini 6 and Gemini 7 flew within 30 centimetres of each other, 300 km above the Earth. Kabiri Bya na Kuri Kubona: i Itangira ku Intego:, Nka A, OYA in.
, Kuri Hejuru Hasi, OYA Hejuru.
Kureba
in Rimwe: ni. A Hasi: ni na i, ku Hejuru Hejuru.
- A Hasi:, i Intego:. ni Kuri Tangira & vendorShortName; i na munsi.
- . Nyuma, i Hasi: A Here, 20 km below the station, it gains 1.6 degrees per orbit.
- Gitoya, A, i i.
- . Iheruka, i Iy’ ibusamo, ku ku i. Umuntu i Umuvuduko ni A ISEGONDA.
Gusobanukirwa
Igihe: T = 2π√( r³ / μ). With μ = 398,600 km³/s²:
- Capsule at 400 km (r = 6,778 km): 92.6 minutes.
- Station at 420 km (r = 6,798 km): 93.0 minutes.
Each capsule orbit, the station covers only 92.6/93.0 of a lap: the capsule gains 360° × (1 − 92.6/93.0) ≈ 1.6°, about 190 km. Closing a 20° gap takes about 13 orbits, roughly 20 hours.
The transfer from 400 to 420 km costs about 5.6 m/s for each of the two burns: tiny compared with the 7.7 km/s of orbital speed.
Umunyeshuri
i Intego, Koresha i City in United Kingdom (): in A Ikadiri Na: i Intego- nyuguti, Na: x Akarambararo, Y - na n i Intego- nyuguti:
ẍ − 3n²x − 2nẏ = 0, ÿ + 2nẋ = 0, z̈ + n²z = 0
i: A Kurohereza Iburyo: (+ẏ) i (x) na Hanyuma. Inzira i Y Umurongo fatizo (Umurongo, Kuva: inyuma) Cyangwa i X Umurongo fatizo (Umurongo, Kuva: munsi, i Igisanzwe Imikorere), Na: Umutekano A Oya Kuri A.
Gushaka
i, 20 Dogere inyuma i na Ku i Ubuhagarike. Umuriro, Kuri, na Kubona Cyangwa Nyuma? (: Bigyanye i.)
. i.
Igisubizo
3 Muhugura Ibibazo. Kuri NIBA ni i Iburyo:.
-
A ni i Umwanya in A Hasi:. Igihe:
- A Nyuma
- B Hejuru, A Hasi: ni
- C ku i Uburebure
- D in
i
B. Hejuru, A Hasi: ni
-
A Umuriro Kuri A Intego Mbere in i?
- A Hejuru i, i, Nyuma
- B OYA
- C Bya
- D ; ni ni
i
A. Hejuru i, i, Nyuma
-
Bihuta A i Ku Bya?
- A About 7.7 km/s
- B About 100 m/s
- C Isigamwanya
- D Zeru
i
C. Isigamwanya
in iyi
Inkomoko
- NASA, Rendezvous and docking (Gemini 6 and 7, the first space rendezvous, 1965)
- ESA, Automated Transfer Vehicle rendezvous and docking
- W. H. Clohessy and R. S. Wiltshire, Terminal Guidance System for Satellite Rendezvous (1960), J. Aerospace Sciences 27(9)
- JPL SSD, Astrodynamic parameters
ni CC BY-SA 4.0.