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Landing the Propellant Stage of a launcher
KTH, Skolan för teknikvetenskap (SCI), Farkost och flyg, Flygdynamik.
2016 (engelsk)Independent thesis Advanced level (degree of Master (Two Years)), 20 poäng / 30 hpOppgave
Abstract [en]

To reduce the cost of launch, several aerospace companies are exploring the possibility of partly reusable launchers. In order to be reusable with minimum refurbishment cost the reusable part of the launcher has to suffer little damage and land in optimal conditions. In this paper, a guidance algorithm to achieve the return of the reusable vehicle on ground through a vertical landing is described. Different mission scenarios are taken into account and the performance of the guidance algorithm is assessed using a 6 Degrees Of Freedom simulator.

sted, utgiver, år, opplag, sider
2016. , s. 11
Serie
TRITA-AVE, ISSN 1651-7660 ; 2016:62
HSV kategori
Identifikatorer
URN: urn:nbn:se:kth:diva-203308OAI: oai:DiVA.org:kth-203308DiVA, id: diva2:1081980
Eksternt samarbeid
Airbus Safran Launchers
Examiner
Tilgjengelig fra: 2017-03-15 Laget: 2017-03-15 Sist oppdatert: 2017-03-15bibliografisk kontrollert

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Totalt: 888 treff
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