Zobrazeno 1 - 10
of 26
pro vyhledávání: '"W. Fehse"'
Autor:
B. Gaubatz, M. Freund, Beate Berkelmann-Loehnertz, Ottmar Baus, M. Heinzler, Manfred Stoll, Rainer Keicher, Hans-Peter Schwarz, M. Blum, W. Fehse
Publikováno v:
Acta Horticulturae. :211-217
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2b93480b39d4fed1dcc32bd799e39a2c
https://doi.org/10.17660/actahortic.2013.978.23
https://doi.org/10.17660/actahortic.2013.978.23
Publikováno v:
IFAC Proceedings Volumes. 25:331-338
The Rendezvous and Docking System Pre-Development Programme, started in 1989 and concluded in 1992, is an early proof-of-concept of an autonomous RVD onboard system for the various potential European scenarios. On the basis of Hermes and Columbus req
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::84a9451a3e855acd8caecc97c1984af9
https://doi.org/10.1016/s1474-6670(17)49671-6
https://doi.org/10.1016/s1474-6670(17)49671-6
Publikováno v:
Acta Astronautica. 28:31-42
This paper first describes the major design drivers and the key features of the European RendezVous and Docking System Concept. Stemming from technology activities led by the European Space Agency (ESA) with European Industry and National Space Agenc
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::5be934007fa19b275519876b0933b6cd
https://doi.org/10.1016/0094-5765(92)90007-6
https://doi.org/10.1016/0094-5765(92)90007-6
Autor:
Wigbert H. W. Fehse
Publikováno v:
ECC
Automatic rendezvous and docking/berthing operations will be one of the key techniques necessary for the operation of the International Space Station (ISS). Russian, European and Japanese transport vehicles will approach to, mate with, and depart fro
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::0feccb9bdf0cb22c496e7bddb681eae8
https://doi.org/10.23919/ecc.1999.7100103
https://doi.org/10.23919/ecc.1999.7100103
The Rendezvous and Docking System Pre-Development Programme, started in 1989 and concluded in 1992, is an early proof-of-concept of an autonomous RVD onboard system for the various potential European scenarios. On the basis of Hermes and Columbus req
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::67950ca5be5b0f74c304399c0eb39d10
https://doi.org/10.1016/b978-0-08-041715-8.50049-3
https://doi.org/10.1016/b978-0-08-041715-8.50049-3
Publikováno v:
Astrodynamics Conference.
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::2d2afbeeb4f2664f67144f369225ec72
https://doi.org/10.2514/6.1992-4437
https://doi.org/10.2514/6.1992-4437
Publikováno v:
IFAC Proceedings Volumes. 18:287-294
Rendez-vous and docking between two orbiting spacecraft has been studied and validated in-space since already two decades and are therefore wellknown, especially for manned systems . However, recent t rends are to design very different rendez-vous an
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::727ee0d44b6967005bb34e9fc3d32381
https://doi.org/10.1016/s1474-6670(17)60901-7
https://doi.org/10.1016/s1474-6670(17)60901-7
Publikováno v:
Journal of Molecular Structure. 97:263-270
The construction of a semi-automatic MW-MW double resonance spectrometer is described, emphasizing the circuitry for the mirror movement, the role of the coupling irises for the pump- and signal resonator respectively, and the realization of high sen
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::b075af47ffdf51aae53d09561942fde8
https://doi.org/10.1016/0022-2860(83)90202-8
https://doi.org/10.1016/0022-2860(83)90202-8
Rendez-vous and docking between two orbiting spacecraft has been studied and validated in-space since already two decades and are therefore wellknown, especially for manned systems. However, recent trends are to design very different rendez-vous and
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::9f0b16845a0537678eda99638b36103d
https://doi.org/10.1016/b978-0-08-032556-9.50042-9
https://doi.org/10.1016/b978-0-08-032556-9.50042-9
Publikováno v:
SPIE Proceedings.
The need for a small pointing facility for Spacelab experiments weighing up to 200kg and calling for low or medium pointing stability became evident from the evaluation of surveys of potential European Spacelab payloads. The Position and Hold Mount (
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::c8a78e184c337af989363bf8c8876e31
https://doi.org/10.1117/12.959865
https://doi.org/10.1117/12.959865