Sökning: "Low Earth Orbit LEO"
Visar resultat 11 - 15 av 22 uppsatser innehållade orden Low Earth Orbit LEO.
11. Development of a Low Earth Orbit Mission Preliminary Analysis Tool
Master-uppsats, KTH/RymdteknikSammanfattning : The objective of this project is the development of a mission analysis tool for the nanosatellite company GomSpace Sweden. Although there are many existing software, they can be quite complicated and time consuming to use. LÄS MER
12. A feasibility study for a satellite VHF Data Exchange System (VDES)
Master-uppsats, KTH/RymdteknikSammanfattning : Transportation across the globe's oceans increases every year and is expected to keep increasing in the following decades. Consequently, there is a need to establish communication over the horizon through the Automatic Identification System (AIS) and the Very High Frequency (VHF) Data Exchange System (VDES), still in development, to track and communicate with vessels all over the globe regardless of the distance from shore. LÄS MER
13. Laser Orbital Derbis Removal : Studies of Spacecraft Debris Removal Using Ground Based Lasers
Master-uppsats, Luleå tekniska universitet/RymdteknikSammanfattning : Overcrowding of the Low Earth Orbit (LEO) region is a growing problem. Decades of treating this part of space like a scrap yard has caused it to become a hazardous environment for operating satellites. LÄS MER
14. A Thermal Investigation and Comparative Study of the Foresail Missions
Master-uppsats, Luleå tekniska universitet/RymdteknikSammanfattning : Cube Satellite (CubeSat) launches have been on the rise since its first launch in2003. This popularity is mainly due to faster design process and lower launch costs.However, most CubeSats are launched into Low Earth Orbits (LEOs), with nomissions to Geostationary Transfer Orbits (GTOs). However, many mission areplanned for the next half-decade. LÄS MER
15. Konceptuell flygplansdesign : Design av flygplan för luft lanserad satellit
Kandidat-uppsats, KTH/Skolan för teknikvetenskap (SCI)Sammanfattning : Det här kandidatexamensarbetet handlar om att design ett flygplan för raketavfyrning på hög höjd. Raketen ska bära satelliten PICARD som väger 143 kg och ska skjutas upp i omloppsbana runt jorden. Flygplanets nyttolast, raketens massa, är tre ton. LÄS MER