Optimisation of a quantum pair space thruster
The paper addresses the problem of propulsion for long term space missions. Traditionally a space propulsion unit has a propellant mass which is ejected trough a nozzle to generate thrust; this is also the case with inert gases energized by an on-board power unit. Unconventional methods for propulsi...
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| Format: | Article |
| Language: | English |
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National Institute for Aerospace Research “Elie Carafoli” - INCAS
2012-06-01
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| Series: | INCAS Bulletin |
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| Online Access: | http://bulletin.incas.ro/files/dragan_v4_iss_2_full.pdf |