AERO 4907 SPACE DESIGN PROJECT Tarik Kaya tkaya@mae.carleton.ca - - PowerPoint PPT Presentation

aero 4907 space design project
SMART_READER_LITE
LIVE PREVIEW

AERO 4907 SPACE DESIGN PROJECT Tarik Kaya tkaya@mae.carleton.ca - - PowerPoint PPT Presentation

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


slide-1
SLIDE 1

AERO 4907 SPACE DESIGN PROJECT

Carleton University Department of Mechanical and Aerospace Engineering 2010

Tarik Kaya tkaya@mae.carleton.ca Office: 3144ME ; Phone: 5692

slide-2
SLIDE 2

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.

slide-3
SLIDE 3

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.

slide-4
SLIDE 4

2008-09 & 2009-10 PROJECT CULPRIT

  • CULPRIT: CARLETON UNIVERSITY LUNAR PENETRATION

REGOLITH INVESTIGATION TEAM

  • 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

slide-5
SLIDE 5

MISSION PROFILE-1

[1] Launch from Earth [2] SELENE Manoeuvres [3] Polar Orbit Reached

slide-6
SLIDE 6

[4] [5] [6] [7] [8]

[4] Detachment from SELENE-1 [5] Propulsion Module Engaged [6] Propulsion Module Detachment [7] Penetrator Free-fall [8] Impact

MISSION PROFILE-2

[4] Detachment from SELENE [5] Propulsion Module Engaged [6] Propulsion Module Detachment [7] Penetrator Free-fall [8] Impact

[4] [5] [6] [7] [8]

slide-7
SLIDE 7

LUNAR PENETRATOR

slide-8
SLIDE 8

DESIGN TEAM STRUCTURE

Integrator Documentation Budget Mission Analysis Payload Structures Propulsion ADCS Power Thermal C&DH Communications

slide-9
SLIDE 9

HARDWARE AND TESTING

slide-10
SLIDE 10

SOFTWARE TOOLS

– Satellite Tool Kit (STK) – ASTOS, a launch vehicle trajectory analysis program – IDEAS/TMG, for thermal analysis – Pro Mechanica, CFX, MATLAB, ABAQUS etc.

slide-11
SLIDE 11

PDR

This year’s PDR is tomorrow (Wednesday, March 10) Senate Room (6th floor) in Robertson Hall from 9:00 to 16:30