Lekti sa a te ekri pa yon Local Solar System Li se yon manm ekip Fondasyon an epi li ka amelyore pa yon revizè ki kalifye. Èske w gen konesans sou sijè sa a? Suggere un changement
In December 1965 Gemini 6 and Gemini 7 flew within 30 centimetres of each other, 300 km above the Earth. It took two years of theory and practice to get there: the first attempts had shown that flying straight at your target, as a pilot would, does not work in orbit.
In orbit, to catch up you drop down, not speed up.
Look
Everything in orbit follows one rule: lower is faster. A lower orbit is shorter and the spacecraft moves faster along it, so it gains on anything higher up.
- Launch into a lower orbit, behind the target. The capsule is timed to start some way behind the station and slightly below it.
- Phasing. Lap after lap, the lower capsule gains a little. Here, 20 km below the station, it gains 1.6 degrees per orbit.
- Two small burns, a mini Hohmann transfer, lift the capsule into the station’s orbit just behind it.
- Final approach. The last few hundred metres are flown slowly, straight along the flight direction, by computers watched by the crew. At contact the closing speed is a few centimetres per second.
Understand
Orbital period: 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.
Master
Near the target, rendezvous engineers use the Clohessy-Wiltshire (Hill) equations: linearised motion in a frame that orbits with the target, with x radial, y along-track and n the target’s mean motion:
ẍ − 3n²x − 2nẏ = 0, ÿ + 2nẋ = 0, z̈ + n²z = 0
They explain the strange behaviour: a push forwards (+ẏ) makes the chaser rise (x grows) and then drift backwards. Approach paths are designed along the y axis (V-bar, from behind) or the x axis (R-bar, from below, where the natural motion helps brake), with safety rules so that a failed engine never leads to a collision.
Tcheke li
Pretend you are the capsule, 20 degrees behind the station and at the same height. If you simply fire your engine forwards, what happens to your orbit, and do you get closer or fall further behind? (Hint: think about the Hohmann lesson.)
Great. Chalè yo se kote lekòl la ranje.
Konplo rapid
3 kesyon rapid. Chwazi yon repons pou wè si ou gen dwa.
-
A capsule is behind the space station in a slightly lower orbit. Over time it:
- A Falls further behind
- B Catches up, because a lower orbit is faster
- C Stays at the same distance
- D Crashes into Earth
Montre repons lan
B. Catches up, because a lower orbit is faster
-
Why can't a spacecraft just fire its engine forwards to catch a target ahead in the same orbit?
- A Because speeding up raises the orbit, which makes the lap longer, so it falls behind
- B Because engines cannot fire forwards
- C Because of air resistance
- D It can; that is how it is done
Montre repons lan
A. Because speeding up raises the orbit, which makes the lap longer, so it falls behind
-
How fast does a capsule approach the station at the moment of docking?
- A About 7.7 km/s
- B About 100 m/s
- C A few centimetres per second
- D Exactly zero
Montre repons lan
C. A few centimetres per second
Finish line
- Li leson an
- Te fè defi a
- Te pran tès la
Mark the lesson complete to save it to your progress on this device.
Leson an fini. Bon travay!
Up next Coming home: reentryMo nan leson sa a
Fon
- 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
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