Skip to main content
Disciplines
Automotive Business IT + Informatics Construction + Real Estate Electrical Engineering + Electronics Energy + Sustainability Insurance + Risk Finance + Banking Management + Leadership Marketing + Sales Mechanical Engineering + Materials
Events
DE
EN
Books
Journals
Topic Page
Marketing
Start single access now
Access for companies
EXTENDED SEARCH
Log in
Top
Published in:
A Study of Hybrid Airfoil Design Method Read chapter Read first chapter

2019 | OriginalPaper | Chapter

OrbitPlus Open CubeSat Platform Feasibility Study and Preliminary System Design

Authors : Hamed Ahmadloo, Alireza Mazinani, Sara Pourdaraei, MohammadReza Bayat, Mahyar Naderi, Ehsan Sherkatghanad

Published in: The Proceedings of the 2018 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2018)

Publisher: Springer Singapore

Log in

Activate our intelligent search to find suitable subject content or patents.

search-config
loading …

Abstract

Following the commercial trend of space sector and taking advantage of smaller satellites to be launched especially in LEO; OrbitPlus Technology Group began the feasibility study and preliminary system design for a 3U CubeSat which can support a general designed payload in one unit and two other units which filled by essential subsystems. This paper contains the main subsystems initial conditions to support longer orbital lifetime with altitudes higher than 500 (Km) for different types of payload. To have a clear idea on required subsystems, Structural, Command and Data Handling, Telecommunication, Power Generation, Attitude Control, Propulsion and End-of-Life Disposal subsystems have been investigated. This study can be first step of initial detail system design of OrbitPlus CubeSat open platform with respect to specific requirements of different payloads.

Dont have a licence yet? Then find out more about our products and how to get one now:

Springer Professional "Wirtschaft+Technik"

Online-Abonnement

Mit Springer Professional "Wirtschaft+Technik" erhalten Sie Zugriff auf:

  • über 102.000 Bücher
  • über 537 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Finance + Banking
  • Management + Führung
  • Marketing + Vertrieb
  • Maschinenbau + Werkstoffe
  • Versicherung + Risiko

Jetzt Wissensvorsprung sichern!

inform now

Springer Professional "Technik"

Online-Abonnement

Mit Springer Professional "Technik" erhalten Sie Zugriff auf:

  • über 67.000 Bücher
  • über 390 Zeitschriften

aus folgenden Fachgebieten:

  • Automobil + Motoren
  • Bauwesen + Immobilien
  • Business IT + Informatik
  • Elektrotechnik + Elektronik
  • Energie + Nachhaltigkeit
  • Maschinenbau + Werkstoffe




 

Jetzt Wissensvorsprung sichern!

inform now
previous chapter Research on a Modeling Method of Ducted Propulsion System for Vertical Take-Off and Landing Aircraft
next chapter Waveriders Designed for Given Planform Leading Edge Curves
Literature
1.
Ahmadloo H, Zhang J (2017) De-orbiting collision risk assessment and detailed orbital simulation of LEO space debris removal drag sail. In: The 9th asian-pacific conference on aerospace technology and science& the 2nd asian joint symposium on aerospace. Beijing, China, pp 201–215
2.
Alvarez JL, Rice M, Samson JR, Koets MA (2016) Increasing the capability of CubeSat-based software-defined radio applications. In: 2016 IEEE aerospace conference, pp 1–10
3.
Cote K, Gabriel J, Patel B, Ridley N, Taillafer Z, Tetreault S (2011) Mechanical, power and propulsion subsystem design for A Cubesat. Worcester Polytechnic Institute
4.
Fiala P, Vobornik A (2013) Embedded microcontroller system for PilsenCUBE picosatellite. In: IEEE 16th international symposium on design and diagnostics of electronic circuits & systems (DDECS), pp 131–134
5.
James Wells G, Stras L, Jeans TG, Foiisy D (2003) Canada’s smallest satellite: the Canadian advanced nano space experiment (CanX-1). In: Proceedings of the 16th annual AIAA/USU conference on small satellites, Logan, UT, USA, August 2002
6.
Johl S et al (2014) A reusable command and data handling system for university CubeSat missions. In: Department of aerospace engineering & engineering mechanical University of Texas at Austin, Austin TX USA Aerospace Conference. IEEE
7.
8.
Li J et al (2013) Design of attitude control systems for CubeSat-Class Nanosatellite. J Control Sci Eng 2013:15CrossRef
9.
Marom G (1996) Book review: advanced composite materials. In: Pilato LA, Michno MJ. Springer Verlag (1994), p 208 + xvii. Price: DM 138.00. ISBN 3-540-57563-4. Heterogeneous Chemistry Reviews 3(1):75–75
10.
Melone CW (2009) Preliminary design, simulation, and test of the electrical power subsystem of the TINYSCOPE Nanosatellite. M.S. Thesis, Naval Postgraduate School, Monterey, CA, USA, December 2009
11.
Pourdaraei S, Qin H, Jin T, Naderi M (2017) High earth orbit navigation by vector tracking. In: 68th International Astronautical Congress (IAC2017), Adelaide, SA, Australia: International Astronautical Federation, IAF
12.
Naderi M, Liang G, Karimi H (2017) Modular simulation software development for liquid propellant rocket engines based on MATLAB Simulink. In: International conference on mechanical, material and aerospace engineering (2MAE). Hong Kong society of mechanical engineers (HKSME), Beijing, China, 12–14 May, 2017
13.
Naderi M, Liang G, Karimi H (2017) Modeling and simulation of staged combustion cycle LPRE. In: 8th international conference on mechanical and aerospace engineering (ICMAE). IEEE Xplore, Prague, Czech Republic
14.
15.
Poghosyan A, Golkar A (2017) CubeSat evolution: analyzing CubeSat capabilities for conducting science missions. Prog Aerosp Sci 88:59–83CrossRef
16.
17.
Reyes G, Kang H (2007) Mechanical behavior of lightweight thermoplastic fiber–metal laminates. J Mater Process Technol 186(1–3):284–290CrossRef
18.
Sabri SF, Yuhaniz SS, Kamardin K (2016) Designing a low-cost CubeSat’s command and data handling subsystem kit. ARPN J Eng Appl Sci 11(10):6259–6264
19.
Sangregorio M et al (2016) Orbital simulation of low-cost drag sail sub-system designed for LEO space debris removal. J Beijing Inst Technol 25(2):15–20
20.
21.
Sokolova O, Carradò A, Palkowski H (2011) Metal-polymer–metal sandwiches with local metal reinforcements: a study on formability by deep drawing and bending. Compos Struct 94(1):1–7CrossRef
22.
Sherkatghanad E, Lang L, Liu S, Wang Y (2017) Innovative approach to mass production of fiber metal laminate sheets. Mater Manufact Process 33(5):552–563CrossRef
23.
24.
Zafar R, Lang L, Zhang R (2014) Experimental and numerical evaluation of multilayer sheet forming process parameters for lightweight structures using innovative methodology. Int J Mater Form 9(1):35–47CrossRef
Metadata
Title
OrbitPlus Open CubeSat Platform Feasibility Study and Preliminary System Design
Authors
Hamed Ahmadloo
Alireza Mazinani
Sara Pourdaraei
MohammadReza Bayat
Mahyar Naderi
Ehsan Sherkatghanad
Copyright Year
2019
Publisher
Springer Singapore
Book
The Proceedings of the 2018 Asia-Pacific International Symposium on Aerospace Technology (APISAT 2018)

Print ISBN: 978-981-13-3304-0

Electronic ISBN: 978-981-13-3305-7

Copyright Year: 2019

DOI
https://doi.org/10.1007/978-981-13-3305-7_97

Premium Partner

    Image Credits