Airship-assisted space launch.
| dc.contributor.author | Guenov, Marin D. | - |
| dc.contributor.author | Peyron, Vincent | - |
| dc.date.accessioned | 2011-11-13T23:30:06Z | |
| dc.date.available | 2011-11-13T23:30:06Z | |
| dc.date.issued | 2004-03-01T00:00:00Z | - |
| dc.description.abstract | Introduction Being lighter-than-air, airships do not seem to be an obvious platform choice for dropping of heavy objects. We have challenged the idea and this paper presents the summary of a speculative concept which utilises airships as a reusable first stage of a space launch system. The inspiration behind the concept was that if not much cheaper, the airship-assisted space launch will be environmentally friendlier- an argument which is likely to become even more important with time. During the development of the concept we have used as a base for comparison the Orbital Sciences Corp. Pegasus XL concept, which is currently the single operational aircraft-based space launch system. Alongside the challenges of estimating weight and cost of the very large airship required (approximately 728,000 m 3 ), the work presented in this paper concentrates mainly on the process of releasing the space launch vehicle from the airship. | en_UK |
| dc.identifier.citation | Marin D. Guenov and Vincent Peyron, Airship-assisted space launch, Airship, March 2004, (143), pp.14-17. | - |
| dc.identifier.uri | http://dspace.lib.cranfield.ac.uk/handle/1826/2987 | |
| dc.title | Airship-assisted space launch. | en_UK |
| dc.type | Article | - |