「Delta v」の共起表現(1語右で並び替え)

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共起表現

「Delta v」の共起表現一覧(1語右で並び替え)

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When designing a trajectory,	delta-v budget is used as a good indicator of how muc
mplies that even small improvements in rocket	delta-v can make large improvements in the size of pr
The	delta-v for a spacecraft rendezvous with this asteroi
very simple way to provide the last necessary	delta-v for those elements on the retro side of the s
For example, the required	delta-v for a Hohmann transfer orbit from the Earth t
Reducing the	delta-v from 3.61 to 2.08 km/s can reduce the total m
I think there wasn't quite enough	delta-V in the LEM available to do the direct abort w
ropellant usage is an exponential function of	delta-v in accordance with the rocket equation, it wi
For example, at 150,000 km, required	delta-v is now 2.17 km/s.
In general physics,	delta-v is simply the change in velocity.
	Delta-v is also required to keep satellites in orbit
In the absence of an atmosphere, the	delta-v is typically the same for changes in orbit in
o full reversal of events, both ways the same	delta-v is used and the same mass ratio applies.
launch typically adds 1,500-2,000 m/s to the	delta-v launch vehicle required to reach normal LEO o
Because the	delta-v needed to achieve the mission usually varies
iderable study is put into reducing the total	delta-v needed for a given spaceflight, as well as de
eping maneuvers are necessary, amounting to a	delta-v of approximately 50 m/s per year.
asteroid of its size from Earth, requiring a	delta-v of only 5.1 km/s for a spacecraft to rendezvo
Commonly space-flight principles including	Delta-V, Orbital insertion and Aerobraking are used t
ft missions, including OSIRIS, due to the low	delta-v required to reach it from Earth orbit.
matic; once rendezvous has been achieved, low	delta-v return windows can be fairly far apart (more
At higher still orbits the required	delta-v rises again.
and may, in certain situations, require less	delta-v than a Hohmann transfer.
transfer may require a lower amount of total	delta-v than a Hohmann transfer in situations where t
e.g. a geostationary orbit, requires a larger	delta-v than an escape orbit, although the latter imp
The speed is 7.8 km/s, the net	delta-v to reach this orbit is 8.0 km/s.
The	delta-v to return from them are usually quite small,
300 m/s) of	delta-V using the OMS.
000 km high Mars gate orbit instead, required	delta-v would be only 2.08 km/s.

共起表現

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「Delta v」の共起表現一覧(1語右で並び替え)