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British scientists achieve plasma ignition in fusion rocket engine prototype

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What specific technical parameters or metrics were achieved during the plasma ignition test?
How does this plasma ignition compare to other fusion experiments in terms of temperature, duration, or energy output?
What is the timeline for developing a functional fusion rocket engine based on this prototype?
What are the main technical challenges remaining before fusion propulsion can be implemented in actual spacecraft?
How much funding or investment has Pulsar Fusion secured for this project, and what are the estimated costs for further development?
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