MARS / Europa InPPS flagship high power space transportation
- NázevTitle
- MARS / Europa InPPS flagship high power space transportationMARS / Europa InPPS flagship high power space transportation
- Druh výsledkuResult type
- Příspěvek ve sborníkuProceedings paper
- AutořiAuthors
- F. Jansen, B. Bergmann, T. Brandt, F. Damme, S. Pospíšil, I. Štekl
- Klíčová slovaKeywords
- Human & Non-human High Power Space Transportation Hybrid Space Tug
- KonferenceConference
- Proceedings of the International Astronautical Congress, IAC (Washington, D.C., 2019-10-21)
- Časopis / citaceJournal / citation
- In: Proceedings of the International Astronautical Congress, IAC, International Astronautical Federation (IAF), 2019 · ISSN 0074-1795
- RokYear
- 2019
- JazykLanguage
- eng
- ZáznamyRecords
- ProjektProject
- Institucionální podpora na rozvoj výzkumné org.Institucionální podpora na rozvoj výzkumné org.
- Citace ke staženíDownload citation
- TXT · BibTeX
AbstraktAbstract
This paper explicitly explains INPPS (International Nuclear Power and Propulsion System) flagship subsystems like nuclear reactor, shielding, power conversion, boom, radiators, building blocks for tanks / payload basket / PPU / cluster of electric thrusters as well as additional solar power ring electricity and real time radiation detectors. Differences between the two flagships - as high power space transportation tug - for non-human (second half of 2020th) Mars / Europa and human (2030th) Mars exploration missions are sketched. The international studied conditions for human Mars and exploration Europa space flights are realizable by rationales for pursuing high power space transportation by INPPS due to: 1) the successful finalization of the European-Russian DEMOCRITOS and MEGAHIT projects with their three concepts of space, ground and nuclear demonstrators for INPPS realization (reached in 2017), 2) the successful ground based test of the Russian nuclear reactor with 1MWel plus important heat dissipation solution via droplet radiators (confirmed in 2018), 3) the space qualification of the Russian reactor until 2025 and 4) the perfect celestial constellation for a Earth-Mars/Phobos-Earth-Jupiter/Europa trajectory in 2026-2035 for most maximal INPPS flagship tests. Critical performance will be studied by parallel realizations of the ground and nuclear demonstrators of DEMOCRITOS (until 2025).
This paper explicitly explains INPPS (International Nuclear Power and Propulsion System) flagship subsystems like nuclear reactor, shielding, power conversion, boom, radiators, building blocks for tanks / payload basket / PPU / cluster of electric thrusters as well as additional solar power ring electricity and real time radiation detectors. Differences between the two flagships - as high power space transportation tug - for non-human (second half of 2020th) Mars / Europa and human (2030th) Mars exploration missions are sketched. The international studied conditions for human Mars and exploration Europa space flights are realizable by rationales for pursuing high power space transportation by INPPS due to: 1) the successful finalization of the European-Russian DEMOCRITOS and MEGAHIT projects with their three concepts of space, ground and nuclear demonstrators for INPPS realization (reached in 2017), 2) the successful ground based test of the Russian nuclear reactor with 1MWel plus important heat dissipation solution via droplet radiators (confirmed in 2018), 3) the space qualification of the Russian reactor until 2025 and 4) the perfect celestial constellation for a Earth-Mars/Phobos-Earth-Jupiter/Europa trajectory in 2026-2035 for most maximal INPPS flagship tests. Critical performance will be studied by parallel realizations of the ground and nuclear demonstrators of DEMOCRITOS (until 2025).