Zobrazeno 1 - 10
of 12 917
pro vyhledávání: '"Roberts, Peter A."'
Autor:
Roberts, Peter1 peter.roberts@canterbury.ac.nz
Publikováno v:
Studies in Philosophy & Education. Apr2024, Vol. 43 Issue 2, p217-221. 5p.
Autor:
Cushen, Alexander T., Oiko, Vitor T. A., Smith, Katharine L., Crisp, Nicholas H., Roberts, Peter C. E., Romano, Francesco, Papavramidis, Konstantinos, Herdrich, Georg
The testing of atmosphere-breathing electric propulsion intakes is an important step in the development of functional propulsion systems which provide sustained drag compensation in very low Earth orbits. To make satellite operations more sustainable
Externí odkaz:
http://arxiv.org/abs/2406.06299
Autor:
Reveley, James1 jreveley@uow.edu.au
Publikováno v:
Studies in Philosophy & Education. Apr2024, Vol. 43 Issue 2, p211-215. 5p.
Autor:
Stuempfle, Stephen
Publikováno v:
NWIG: New West Indian Guide / Nieuwe West-Indische Gids, 2019 Jan 01. 93(1/2), 126-127.
Externí odkaz:
https://www.jstor.org/stable/26742419
Autor:
Toh, Glenn1 GKPToh@ntu.edu.sg
Publikováno v:
Educational Philosophy & Theory. Jul2024, Vol. 56 Issue 8, p816-818. 3p.
Autor:
Roberts, Peter1 peter.roberts@canterbury.ac.nz
Publikováno v:
Studies in Philosophy & Education. Sep2020, Vol. 39 Issue 5, p573-575. 3p.
Autor:
Chen, Rosa Hong1 rosachen0921@gmail.com
Publikováno v:
Studies in Philosophy & Education. Sep2020, Vol. 39 Issue 5, p569-571. 3p.
Autor:
Longa, Rachel1 rachel.longa@gmail.com, Fortier, Nicholas2
Publikováno v:
Studies in Philosophy & Education. Sep2020, Vol. 39 Issue 5, p565-567. 3p.
Autor:
Franicevic Jared
Publikováno v:
The Journal of World Energy Law & Business. 15:74-75
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_________::a4037c6ad6d906e55d3887f07f2971f4
https://doi.org/10.1093/jwelb/jwab036
https://doi.org/10.1093/jwelb/jwab036
Autor:
Livadiotti, Sabrina, Crisp, Nicholas H., Roberts, Peter C. E., Oiko, Vitor T. A., Christensen, Simon, Dominguez, Rosa Maria, Herdrich, Georg H.
This paper discusses the design and the performance achievable with active aerodynamic attitude control in very low Earth orbit, i.e. below 450 km in altitude. A novel real-time algorithm is proposed for selecting the angles of deflection of aerodyna
Externí odkaz:
http://arxiv.org/abs/2203.07790