The strategic issues with implementing open avionics platforms for spacecraft

IEEE Aerospace Conference Proceedings

Volumn 4, Issue , 2002, Pages 1825-1841

  Caffrey, Robert T ^a   Simpson, Timothy W ^b   Henderson, Rebecca ^c   Crawley, Edward ^d  

^a NASA GODDARD SPACE FLIGHT CENTER   (United States)

^b The Pennsylvania State University   (United States)

^c MASSACHUSETTS INSTITUTE OF TECHNOLOGY   (United States)

^d Massachusetts Institute of Technology   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ORGANIZATIONS; DEVELOPMENT CYCLE; MANUFACTURING PROCESS; NON-AEROSPACE INDUSTRY; OPERATING ENVIRONMENT; SPACECRAFT AVIONICS; SPACECRAFT SYSTEM; STRATEGIC BENEFITS;

AEROSPACE INDUSTRY; AVIONICS; COMPUTER SOFTWARE REUSABILITY; CONSUMER ELECTRONICS; PRODUCT DEVELOPMENT; SPACECRAFT;

SPACE FLIGHT;

EID: 84879360136     PISSN: 1095323X     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.1109/AERO.2002.1036895     Document Type: Conference Paper

References (37)

1. Baldwin, C.Y.Clark, K.B.(2000), Design Rules: The Power of Modularity, MIT Press, Cambridge, MA
2. Gonzalez-Zugasti, J., Otto, K., Baker, J. (1998), A Method for Architecturing Product Platforms with an Application to lnterplanetaiy Mission Design, Proceedings of 1998 DETC: 1998 ASME Design Automation Conference
3. Gordon Johnston Interview, former NASA Headquarters manager in the ESSP Program Office, 10/00
4. Spears, A.J., (March 2000), NASA FBC Task, NASA Headquarters
5. Hanratty, J., Lightsey, R., Larson, A., (1998), Open Systems and the System Engineering Process, http://www.acq.osd.mil/os jtf-
6. Ruffa, Castell, Flatley, and Lin (1998), MIDEX Advance Modular and Distributed Spacecraft Avionics Architecture, IEEE Aerospace Conference Proceedings
7. Strope, D (1996), X-Ray Timing Explorer (XTE), A Standard of Excellence, Internal NASA Report
8. Fraeman, M. (1997), A Fault Tolerant Integrated Electronics Module for Small Satellites, llthAIAA/USU Conference on Small Satellites
9. Langlois R. (1999), Modularity in Technology, Organization, and Society, Austrian Economics and the Theory of the Firm
10. Ulrich, K.T. Eppinger, S.D.(2000), Product Design and Development, McGraw Hill
11. Christensen and Verlinden (2000), Disruption, Disintegration, and the Dissipation of Differentiability, In Press
12. Henderson, R.,(1999), Class Tape, Technology Strategy Class, Class #2, #3, #6, and #8
13. Shapiro and Varian (1999), Information Rules, Harvard Business School Press, Cambridge, MA.
14. Caffrey, Hestnes, Cuviello, and Shaw (1997), A Standard Spacecraft Data System on a Chip: NASA Goddard Space Flight Center's Essential Services Node (ESN), 1997 IEEE Aerospace Conference Proceedings
15. Rick Fleater Interview, 12/22/00, AeroAstro CEO (Micro Satellite Vendor)
16. Meyer H. and Lehnerd A. (1997), The Power of Product Platform: Building Value and Leadership, The Free Press
17. Caffrey, R., Simpson, T., Henderson, R., Crawley, E., (2002) The Technical Issues with Implementing Open Avionics Platforms for Spacecraft, 4ffh AIAA Aerospace Science Meeting, Reno, NV, January 2002
18. Schulz, A., Fricke, E Igenbergs, E (7/2000), Enabling Changes in Systems throughout the Entire Life-Cycle-Key to Success?, Proceeding of 10th Annual Symposium of INCOSE, Minneapolis
19. Suh N., (1990), The Principles of Design, Oxford University Press, Oxford, UK.
20. Lyke, J., (1998), Open Systems and Their Applicability to the Advanced Sensor and Discriminating Interceptor Technology Programs (ASTP/DITP), White Paper, Air Force Research Laboratory, Albuq., NM
21. Caffrey, R. (2001), Implementing Spacecraft Avionics Platforms based on an Open Architecture, MIT Masters Thesis
22. Roberson and Ulrich, K.T. (September 1998), Planning Product Platforms, Sloan Management Review, Vol. 39(4)
23. Simpson, T. W., Maier, J. R. A. and Mistree, F. (2001) Product Platform Design: Method and Application, Research in Engineering Design, Vol. 13(1), pp. 2-22. (Pubitemid 33046252)
24. Mr. Fitzpatrick presentation, former Boeing Project Manager, Presentation to Manufacturing Class, MIT, (7/00)
25. Steve Dorfman interview, former CEO of Hughes Space and Communication, MIT, (10/16/00)
26. Wray, R. and Stovall, J. (1993), Space Generic Open Architecture (SGOAA) Standard Specification, LESC-3054-B
27. Marshal, J., Belvin, S., Laurvick, C. (1995), Creating Scaleble, Reusable, Interoperable, Spaceborne Computer Modules with a High Performance Backplane Bus, AIAA Computing in Aerospace 10, AIAA-95-1005-C
28. (April 3, 1995 ), New Techniques Allow 22-Day Satellite Assembly, Aviation Week and Space Technology, Vol 142, #14
29. Borky, J., Singaraju, B.K., Stevens, K. (1996), An Advanced Spacecraft Avionics Architecture, IEEE, 07803-3196-6/96
30. Watzin, J. (1998), SMEX-Lite-An Innovative System Architecture for Reducing Spacecraft Size and Cost, 49'h International Astronautical Congress
31. Chau, S. et. al. (2000), The Implementation of a COTS Based Fault Tolerant Avionic Bus Architecture, IEEE Aerospace Conference
32. Galeazzi, C. (2000), PRIMA: A New, Competitive Small Satellite Platform, Acta Astronáutica, Vol. 46
33. Hult, T., Linder, B. (2000), Towards a Single Platform Electronic Unit in a Shoe-box, AIAA Space 2000 Conference & Exposition
34. Durteste, C., Schirmann, T., Dribault, L. (2000), The LEOSTAR Solution for High Performance Earth Observation Missions, Acta Astronáutica, Vol. 46, Nos. 2-6
35. Wahl, Z., Walker, K., Ward, J., (2000), Modular and Reusable Miniture Subsystems for Small Satellite An Example Describing Surry's Nanosatellite S-Band Downlink, 11th AIAA/USU Conference on Small Satellites
36. (5/21/99), Interface Requirements Document (IRD) for the National Polar-orbiting Operational Environmental Satellite System (NPOES), NPOES Integrated Program Office
37. S-415-202 (9/25/00), The Advanced Baseline Imager (ABI), Request for Proposal (RFP), Attachment A, Statement of Work (SOW)