Pages that link to "Item:Q370536"
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The following pages link to The effect of the elasticity of an orbital tether system on the oscillations of a satellite (Q370536):
Displaying 10 items.
- Dynamics of towed large space debris taking into account atmospheric disturbance (Q405052) (← links)
- The oscillations of a satellite probe towed on an inextensible line in an inhomogeneous atmosphere (Q917349) (← links)
- Analysis of the dynamics of the formation of a tether group of three nanosatellites taking into account their motion around the centers of mass (Q2070797) (← links)
- Nonperiodic oscillations of micro- and nanostrings in a gaseous medium (Q2086758) (← links)
- Spin-orbital resonance motion of a satellite with two flexible viscoelastic rods in an elliptical orbit (Q2226149) (← links)
- Linear transverse oscillations of the space elevator cable (Q2656467) (← links)
- Dynamics of a space vehicle with elastic deploying tether (Q4513637) (← links)
- (Q4905053) (← links)
- MATHEMATICAL SIMULATION OF A TETHERED SATELLITE SYSTEM MOTION WITH AN INFLATABLE SPHERICAL BALLOON DURING A SPACECRAFT ORBIT INJECTION (Q5042930) (← links)
- On the dynamics of deployment of an orbital structure with elastic elements (Q5294499) (← links)
