AERO 4907 SPACE DESIGN PROJECT Tarik Kaya tkaya@mae.carleton.ca Office: 3144ME ; Phone: 5692 Carleton University Department of Mechanical and Aerospace Engineering 2010
2004-05 & 2005-06 PROJECT AEGIS AEGIS (Air-launched Earth-observing Ground Information System) • Primary Mission Objective: • – To design a low cost air-launch vehicle and micro satellite for the purpose of earth observation.
2006-07 & 2007-08 PROJECT NORSAT Primary Mission Objectives: • – To design a low cost micro satellite(s) mission for observation of Canada’s Arctic region, and the distribution of the information in a timely manner. – Space, launch and ground segments will be considered.
2008-09 & 2009-10 PROJECT CULPRIT • CULPRIT: C ARLETON U NIVERSITY L UNAR P ENETRATION R EGOLITH I NVESTIGATION T EAM Mission Statement: “To design a micro-penetrator to survive • lunar impact and report upon the characteristics of the sub- surface regolith “ Mission Objectives: • Primary: To survive as a tech demo and report on impact characteristics Secondary: To detect water on the moon
MISSION PROFILE-1 [1] Launch from Earth [2] SELENE Manoeuvres [3] Polar Orbit Reached
MISSION PROFILE-2 [4] [4] [5] [5] [6] [6] [4] Detachment from SELENE [4] Detachment from SELENE-1 [7] [7] [5] Propulsion Module Engaged [5] Propulsion Module Engaged [8] [8] [6] Propulsion Module Detachment [6] Propulsion Module Detachment [7] Penetrator Free-fall [7] Penetrator Free-fall [8] Impact [8] Impact
LUNAR PENETRATOR
DESIGN TEAM STRUCTURE Integrator Communications Mission Analysis Documentation C&DH Payload Thermal Structures Budget Power Propulsion ADCS
HARDWARE AND TESTING
SOFTWARE TOOLS – Satellite Tool Kit (STK) – ASTOS, a launch vehicle trajectory analysis program – IDEAS/TMG, for thermal analysis – Pro Mechanica, CFX, MATLAB, ABAQUS etc.
PDR This year’s PDR is tomorrow (Wednesday, March 10) Senate Room (6th floor) in Robertson Hall from 9:00 to 16:30
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