CognitiveNet
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Ion Thrusters which are used for space vessels, such as sending sattelites into space, how much do they cost?
The discussion revolves around the costs associated with ion thrusters used in space vessels, particularly for launching satellites. Participants explore various factors influencing pricing, technical specifications, and the feasibility of using ion thrusters for specific missions.
Participants express differing views on the capabilities of ion thrusters, particularly regarding their use for launching satellites and the associated costs. There is no consensus on the feasibility of using ion thrusters for specific missions or the accuracy of the calculations presented.
Some participants' calculations depend on assumptions about gravitational forces and thrust requirements, which may not be universally accepted or applicable in all scenarios. The discussion includes speculative elements regarding the performance of ion thrusters in various contexts.
Simon Bridge said:Depends on the spacecraft and it's mission.
Never heard of off-the-rack ion drives.
iirc: costs can range from 10's of thousands to milions per unit.
What is your interest.
See :
http://www.boeing.com/defense-space/space/bss/factsheets/xips/xips.html
http://www.aerojet.com/capabilities/ spacecraft .php
CognitiveNet said:I have a reactor which produces 100KW and weights about 500Kg.
Simon Bridge said:Well then approach the manufacturers and tell them your requirements - what are you messing with us for??!
Note: the thruster will accelerate your craft for as long as it has power and fuel ... there is no theoretical top speed...
Ion thrusters capable of sending satellites into space do not exist. Thrust to weight ratio of modern ion thrusters is very low, making them impossible to use until you have at least established an orbit.CognitiveNet said:Ion Thrusters which are used for space vessels, such as sending sattelites into space
CognitiveNet said:I must ask. Since the minimum required thrust to escape Earth is 9,81N/Kg, and I wanted to accelerate 10m/s^2, I would need a thrust of 19,81N/Kg. If my spaceship weights 300Kg, I would need a thrust of (10+9,81)*300= 5943 Newton. After 4 minutes and 38 seconds I would be traveling at 10'000km/h. So my question is, if you would be in empty space, the thrust required in order to reach the same velocity from 0km/h, would be equivalent to 10m/s^2 + 0m/s^2, because there is nothing dragging you down. Is this correct?