Výsledky vyhledávání - "ZANDBERGEN, B.T.C."

Akademický článek

Cost estimating of commercial smallsat launch vehicles

Autor: Drenthe, N.T., Zandbergen, B.T.C., Curran, R., Van Pelt, M.O.

Publikováno v: In Acta Astronautica February 2019 155:160-169

Student perceptions on a collaborative engineering design course

Autor: van Helden, G., Zandbergen, B.T.C., Specht, M.M., Gill, E.K.A., Jarvinen, Hannu-Matti, Silvestre, Santiago, Llorens, Ariadna, Nagy, Balazs Vince

Publikováno v: Proceedings of the 50th Annual Conference Universitat Politècnica de Catalunya · BarcelonaTech (UPC)

To adequately prepare engineering students for their professional career, educational institutions offer projects in which students collaboratively solve engineering design problems. It is known from research these projects can lead to a variety of l

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f1e729e3e7bf3242e26e2fbaceed3c3a
https://doi.org/10.5821/conference-9788412322262.1323

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Design of a 1-N monopropellant thruster for testing of new hydrogen peroxide decomposition technologies

Autor: Franken, Thim, Valencia-Bel, Ferran, Jyoti, B.V.S., Zandbergen, B.T.C.

Publikováno v: Aerospace Europe Conference 2020; BORDEAUX, FRANCE, 25-28 February 2020

Since there is a high interest in the use of green propellants, hydrogen peroxide is coming back after once making place for the rise of Hydrazine in monopropellant propulsion systems. Typically, these thrusters are outfitted with catalyst beds. A fu

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=narcis______::53765830511f0589f92fc15ffc575f9d
http://resolver.tudelft.nl/uuid:16ae861e-1600-4bff-a853-57108e35d1cc

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Laser Ignition and Combustion Study of KNO3-Sorbitol based Solid Propellant

Autor: OLDE, M.C., ZANDBERGEN, B.T.C., JYOTI, B.V.S., VAN DEN WIJNGAART, J.A.B.J., KUHNERT, F.A., VAN SLINGERLAND, J.

KNO3 -Sorbitol (KNSB) is a simple, cheap and safe solid propellant that is used extensively in the student and amateur rocketry communities. During Ballistic Evaluation Motor (BEM) tests with different propellant compositions it was found that igniti

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=doi_________::f4708c30b3354f83a751bc8b72487e34

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Akademický článek

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Cryogenic rocket engine development at Delft aerospace rocket engineering

Autor: Wink, J, Hermsen, R., Huijsman, R, Akkermans, C., Denies, L., Barreiro, F., Schutte, A., Cervone, A., Zandbergen, B.T.C.

Publikováno v: Space propulsion 2016

This paper describes the current developments regarding cryogenic rocket engine technology at Delft Aerospace Rocket Engineering (DARE). DARE is a student society based at Delft University of Technology with the goal of being the first student group

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=narcis______::905eb370aa1937219e739d92861468bb
http://resolver.tudelft.nl/uuid:079c6df4-f136-4efd-bb26-7c1d4983463e

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Green micro-resistojet research at Delft University of Technology: the new frontiers of Cubesat propulsion

Autor: Cervone, A., Zandbergen, B.T.C., Cordeiro Guerrieri, D., de Athayde Costa e Silva, M., van Zeijl, H.W.

Publikováno v: CEAS Space Journal, 9(1)

The aerospace industry is recently expressing a growing interest in green, safe and non-toxic propellants for the propulsion systems of the new generation of space vehicles, which is especially true in the case of Cubesat micro-propulsion systems. De

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=narcis______::daf981c7e95cec2b4d04d01e24157a45
http://resolver.tudelft.nl/uuid:c19e0af5-923d-4e11-9c82-1aea5059b472

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Heater Chip with Different Microchannels Geometries for a Low Pressure Free Molecular Micro-Resistojet

Autor: Cordeiro Guerrieri, D., de Athayde Costa e Silva, M., Zandbergen, B.T.C., Cervone, A.

Publikováno v: Space propulsion 2016

This paper presents a dynamic system approach for the modeling of fluid flow in microchannels to be used in thrust control applications. A micro-resistojet fabricated using MEMS (Microelectromechanical Systems) technology has been selected for the an

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=narcis______::e15d0256b93ab8893df945cc1a1aa10d
http://resolver.tudelft.nl/uuid:00545557-b420-4634-a143-399434da899b

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Design, Fabrication, Testing and Modeling of a Vaporizing Liquid Micro-Propulsion System

Autor: van Wees, T., Hanselaar, C.A.J., Jansen, E, Cervone, A., Zandbergen, B.T.C., van Zeijl, H.W.

Publikováno v: Space propulsion 2016

In the last decade, CubeSat development has shown the potential to allow for low-risk, low-cost space missions. To further improve the capabilities of CubeSats in large scale missions, a novel micro-propulsion system is being developed at Delft Unive

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=narcis______::267ec171d5d0ebe01e2e45cc6a49f302
http://resolver.tudelft.nl/uuid:9811010e-75a8-4146-8175-b8c454c43d20

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Development and Performance of the 10 kN Hybrid Rocket Motor for the Stratos II Sounding Rocket

Autor: Werner, R.M., Knop, T.R., Wink, J, Ehlen, J, Huijsman, R, Powell, S, Florea, R., Wieling, W, Cervone, A., Zandbergen, B.T.C.

Publikováno v: Space propulsion 2016

This paper presents the development work of the 10 kN hybrid rocket motor DHX-200 Aurora. The DHX-200 Aurora was developed by Delft Aerospace Rocket Engineering (DARE) to power the Stratos II and Stratos II+ sounding rocket, with the later one being

Externí odkaz: https://explore.openaire.eu/search/publication?articleId=narcis______::c5674e92373de2775ac4d505516e065e
http://resolver.tudelft.nl/uuid:212a6612-a090-4076-9833-e4e3e675b0ee

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