Nanospace-1: The impacts of the first swedish nanosatellite on spacecraft architecture and design

Acta Astronautica

Volumn 53, Issue 4-10, 2003, Pages 633-643

  Bruhn, Fredrik ^a   Köhler, Johan ^a   Stenmark, Lars ^a  

^a UPPSALA UNIVERSITY   (Sweden)

Author keywords

[No Author keywords available]

Indexed keywords

DEGREES OF FREEDOM (MECHANICS); FUNCTIONS; RISK ASSESSMENT; SATELLITES; STRUCTURAL PANELS; SYSTEMS ANALYSIS;

NANOSATELLITES; SPACECRAFT ARCHITECTURE; SYSTEM ASSEMBLY; THERMAL MANAGEMENT;

SPACECRAFT;

EID: 10844248639     PISSN: 00945765     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0094-5765(03)80024-3     Document Type: Article

References (15)

1. The Munin Nanosatellite (2000), http://munin.irf.se
2. R. Chari, Pre-Flight Characteristics of U.S. Air Force Academy's FalconSat-1, 13th Annual AIAA/USU Conference on Small Satellites.
3. Surrey Nanosatellite Technology, SSTL, (2002),(http://www.sstl.co.uk/missions/mn_snap_extra.html)
4. ESTEC Contract No 14905/01/NL/MM, Evalutation and Reliability of Micro Propulsion Systems for Earth Explorer Missions.
5. rd United Nations Conference on the Exploration and Peaceful Uses of Outer Space (1998), A/CONF.194/BP/9.
6. P. Nilsson, M. Jönsson, L. Stenmark (2001), Chip Mounting and Interconnection in Multi Chip Modules for Space Applications, Journal of Micromechanics and Microengineering, 11, 339-343.
7. E.B. Franke, C.L. Trimble, J.S. Hale, M. Schubert, J.A. Woolam (2000), Infrared switching electrochromic devices on tungsten oxide, , J. of Applied Physics 5777,88
8. M. Brogren, G. L. Harding, R. Karmhag, C.-G. Ribbing, G.A. Niklasson, L. Stenmark (2000), Titanium-aluminium-nitride coatings for satellite temperature control, Thin Solids Films, 370, 268-277.
9. L. Klintberg, M. Karlsson, L. Stenmark, J.-Å. Sehweitz, G. Thornell, A large stroke, high force paraffin phase transition actuator, accepted for publication in Sensors and Actuators in August 2001.
10. Bosch, Gmbh, CAN standard, http://www.can.bosch.com
11. Honeywell Inc, Smart Distributed System, (2002),http://content.honywell.com/sensing/prodinfo/sds
12. H. Tiggeler, T. Vladimirova, D. Zheng, J. Gaisler (2000), Experiences Designing a System-on-a-Chip for Small Satellite Data Processing and Control, Proceedings MAPLD00 Military and AeroSpace Applications of Programmable Devices and Technoligies, P-2, Maryland USA
13. J. Köhler, J. Bejhed, H. Kratz, F. Brunn, U. Lindberg, K. Hjort, L. Stenmark (2001), A Hybrid Cold Gas Microthruster System for Spacecraft, Accepted by Sensors and Actuators A.
14. Mehra A., Zhang X., Ayon A.A, Waitz I.A, Schmidt M.A., and Spadaccini C.M. (2000), A 6-Wafer Combustion System for a Silicon Micro Gas Turbine Engine, Journal of MicroElectroMecanical Systems, 18, 517
15. European Space Agency (ESA) Official Homepage,(2002),http://labs.esa.int/labs.php3?lab=concdesfacil