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ISU SSP 2014 | Team Project Proposal | AMOOS Project
René Jr. Landry
18 September 2013
International Space University – Space Studies Program
Team Project Proposal
19/09/2013 1
ISU – SSP 2014 Evening
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 2
OUTLINES
1. INTRODUCTION TO MAIN PROBLEMATICS
2. REVIEW ON SPACE DEBRIS ACTIVITIES
3. REVIEW OF SPACE VEHICLES TECHNOLOGIES
4. GLANCE ON ISU-SSP 2014 AMOOS PROJECT
5. CONCLUSION
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 3
A. Satellites lifetime
B. Space debris
Various Space Debris (Images from OOBJECT and ECLIPSE TOURS )
Dead satellites on graveyard orbits. (Images from US Air Force, public domain)
1. INTRODUCTION TO MAIN PROBLEMATICS
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 4
1. INTRODUCTION TO MAIN PROBLEMATICS
MEO
GEO (35 784 Km)
LEO HEO
A.1 – Satellites Quick Facts
AMOOS PHASE I
(LEO)
AMOOS PHASE II
(MEO / GEO)
MOON ~384 000 Km
~10x GEO
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 5
1. INTRODUCTION TO MAIN PROBLEMATICS
Note : Return trip Montréal-Québec : ~500 Km
LEO : ~200 to 2000km
1 x Mtl to Qc to 4 x Return trip Mtl-Qc
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 6
A.1 – Satellites Quick Facts
Total number of operating
satellites (May 2013) 1071
LEO 523 (48.8%)
MEO 75 (0.07%)
ELLIPTICAL 38 (0.03%)
GEO 435 (40.6%)
(Source: Union of Concerned Scientists, May 2013)
1. INTRODUCTION TO MAIN PROBLEMATICS
Distribution of satellites in different orbits (Union of Concerned Scientists, 2012)
LEO is an important
region for Space/Satellite
Applications
Definition :
Thermosphere : ~80 to 500km (gases drag)
Exosphere : ~500 to 2000km
LEO :
Satellite speed : ~7.8 km/s
Satellite period : ~90min
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 7
Distribution of satellites by applications (Union of Concerned Scientists, 2012)
1. INTRODUCTION TO MAIN PROBLEMATICS
A.1 – Satellites Quick Facts
Estimates of costs factors during
satellites life cycle Cost Range
Conception $50M - $250M
Launch $100M - $200M
Insurance $50M - $150M
Maintenance Multi-millions dollars
Ground monitoring Multi-millions dollars
(Source: EXAMINER, 2009)
Satellite On-Orbit Servicing is
economically and commercially viable !
Several studies: [36]-[41]
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 8
Components failures / limitations
Fuel propellant: limited capacity, loss of fuel
Solar array drive / panels: degradations, malfunctions
Power modules: battery cells failures
Communication modules: redundant anomalies
Antenna: transmitter failures
Payload or Sensor anomalies
Nowadays : ~70%
satellite end-of-life from
lost of energy source
Sources: NORDIC SPACE and LANDSAT
1. INTRODUCTION TO MAIN PROBLEMATICS
A.2 – Potential Subsystems Failures
Satellite End-of-Life Concept
Until the absolute end of its on-board fuel,
or until Power source of spacecraft fails,
or until all on-board instruments fail.
Sources : 13th Annual AIAA/USU Conference on Small Satellites
Constellation End-of-Life Policy January 1998, US DoD 1. LEO will burn within 25 years (re-entry) 2. GEO in graveyard at 36400km
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 9
A.3 – Satellites end-of-life issues
1. INTRODUCTION TO MAIN PROBLEMATICS
Due to these factors:
LEO Satellites have useful on-orbit
lifespan of 1 to 8 years.
LEO Servicing constraints:
Limited maintenance capabilities
High risky repair Manned missions
Interested facts :
Nowadays, satellite technologies
are extremely robust …
LEO Satellites could have :
- a complete new life
- new sources of energy
- new functions
with On-Orbit Servicing !
Hubble Space Telescope
4 Servicing Missions since 1990
Still in operation !
ISU SSP 2014 | Team Project Proposal | AMOOS Project 9/19/2013 10
B. Space debris issues
Feb. 2009, the scene was at 800km above Siberia. In the explosion, Iridium 33 and Kosmos 2251 are completely destroyed.
Generation of ~800 new Space Debris !
In July 1996, le satellite Cerise Satellite was damaged with an Ariane debris (launched
10 years ago)
On March 2008, Jules Verne ATV was launched in LEO. Seven month after,
perfect reentry degradation. Daily manoeuver of the ISS
ISU SSP 2014 | Team Project Proposal | AMOOS Project 9/19/2013 11
B. Space debris issues
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 12
1. INTRODUCTION TO MAIN PROBLEMATICS
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 13
1. INTRODUCTION TO MAIN PROBLEMATICS
Source: NASA
56 years later …
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 14
Source: NORDIC SPACE
B.1 – Evolution of Space Debris
1. INTRODUCTION TO MAIN PROBLEMATICS
FACT 1:
6578 satellites launched since
Sputnik-1 (source UCS, May 2013)
Only ~800 active Satellites today !
FACT 2:
>95% of tracked object
population are debris
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 15
Source: NORDIC SPACE
Space debris population in LEO (2013) :
> 14,000 objects > 10cm
> 300,000 objects 1-10cm
> 30 Million objects < 1cm
1. INTRODUCTION TO MAIN PROBLEMATICS
B.1 – Evolution of Space Debris
Ex.: Kevlar shielding
Tracked with Radar
No tracking, no shielding !
Micro debris : Eye view
Micro debris : Zoom
?
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 16
1. INTRODUCTION TO MAIN PROBLEMATICS
B.1 – Evolution of Space Debris For fifty years, the primary source of all of the junk came from
objects that exploded by accident.
Except Fengyan-1C ! + 3000 new large debris
(intentional anti-satellite test missile)
The Chinese mission was a success !
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 17
Source: Space Academy Australia and Images taken from ECLIPSE TOURS
MAN MADE
Rocket bodies
17%
Mission-related debris
19%
Abandoned spacecraft
22%
Fragmentation debris
42%
Breakup
fragments
Collisional
fragments
Deterioration
products
Exhaust
products
Objects released in
Deployment & Mission Operations
Refuse from
Human Missions
Explosions
B.2 – Sources of Space Debris
Ariane V payload (2009, Mexico) PAM-D debris (2002, Saudi Arabia )
Delta rocket debris(2013, Zimbabwe)
1. INTRODUCTION TO MAIN PROBLEMATICS
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 18
B.3 – Problematic of Space Debris (Part I)
1. INTRODUCTION TO MAIN PROBLEMATICS
Source: Ecolocalizer.com, Null-Hypothesis.co.uk, and Science.nasa.gov
1-mm diameter aluminum sphere moving at a velocity of 10 km/s will pierce a 4-mm thick aluminum wall
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 19
Space debris production and dangers :
In-orbit collisions with other debris or spacecraft
In-orbit explosions
LEO orbit congestions
Hypervelocity collisions and high kinetic energy releases
Smallest debris pass through protection hulls of satellites structures (avg. 10km/sec)
Scattering radioactive fallouts can contaminate the space and ground.
1. INTRODUCTION TO MAIN PROBLEMATICS
B.3 – Problematic of Space Debris (Part II)
Very complex and expensive process to deal with Space Debris !
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 20
Source: Liou, 2011
Space debris generation and population:
Kessler Syndrome (Donald J. Kessler, Nasa)
Unpredictability of small debris collisions
Reduction of Astronaut Outdoor mission
Extension of graveyard orbits
Long debris lifetime in orbits
LEO orbit congestions: Orbital debris increasingly span large space orbit
Difficulty to track smallest orbital debris (< 10cm)
1. INTRODUCTION TO MAIN PROBLEMATICS
B.3 – Problematic of Space Debris (Part III)
In a short term, ISS will become inoperable !
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 21
1. INTRODUCTION TO MAIN PROBLEMATICS
B.3 – Problematic of Space Debris (Part III)
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 22
MISSION
Use of a low cost UAV (Unmanned Aerial Vehicle) for Autonomous On-Orbit Satellite Servicing
MAIN OBJECTIVES
1- To extend satellites lifetime and performance
On-orbit servicing (maintenance, replacement, etc.)
Repair critical satellite faulty subsystem
New energy sources (refuel, battery, solar panel, etc.)
Update functions, missions or add new technology
2- To help removing space debris
Help de-orbiting old satellites or debris
Cargo back on earth
Execute other debris removal techniques
1. INTRODUCTION TO MAIN PROBLEMATICS
AMOOS Project : A Call for Action
3- To bring small payload in space
Put small satellite / payload in orbit
Use the UAV as a scientific laboratory
Great Opportunity :
Significant environment impact
Solution to an urgent
International problem
Several economic outcomes
↑ Canada/ÉTS reputation in
Space Activities
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 23
2. REVIEW ON SPACE DEBRIS ACTIVITIES
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 24
2. REVIEW ON SPACE DEBRIS ACTIVITIES
A. SPACE DEBRIS PROGRAMS
B. CURRENT MITIGATION ACTIVITIES : PREVENTION
C. FUTURE MITIGATION ACTIVITIES : REMOVAL
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 25
ASI
CNES
CNSA
CSA
DLR
ESA
ISRO
JAXA
NASA
SSAU
ROSCOSMOS
UK SPACE
Agenzia Spaziale Italiana
Centre National d'Etudes Spatiales
China National Space Administration
Canadian Space Agency
German Aerospace Center
European Space Agency
Indian Space Research Organization
Japan Aerospace Exploration Agency
National Aeronautics and Space Administration
State Space Agency of Ukraine
Russian Federal Space Agency
UK Space Agency
Source: IADC
A.1 – IADC: Committee Member Organizations
2. REVIEW ON SPACE DEBRIS ACTIVITIES
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 26
Source: IADC
Purpose of IADC Organization:
1) Exchange information about orbital debris research among member space agencies.
2) Review progress of ongoing cooperative activities.
3) Facilitate opportunities for cooperation in space debris research.
4) Identity debris mitigation practices and options.
A.2 – Inter-Agency Space Debris Coordination Committee (IADC) – International Committee
2. REVIEW ON SPACE DEBRIS ACTIVITIES
Deliverables :
Produces the “IADC Space Debris Mitigation Guidelines”.
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 27
European Code of Conduct for Space Debris Mitigation
FCC. Orbital Debris Mitigation Standard Practices
IADC Space Debris Mitigation Guidelines
ITU Environment Protection of the Geostationary Orbit
NASA. Process for Limiting Orbital Debris. NASA-STD-8719.14
NASA. Safety Standard. Guidelines and Assessment Procedures for limiting Orbital Debris
Space Product Assurance. Safety. ECSS-Q-40A
UNCOPUOS. Technical Report on Space Debris
UNCOPUOS. Space Debris
Source: EUTELSAT MITIGATION GUIDELINES 2013
A.3 – International Recommendations and Guidelines
2. REVIEW ON SPACE DEBRIS ACTIVITIES
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 28
2. REVIEW ON SPACE DEBRIS ACTIVITIES
A. SPACE DEBRIS PROGRAMS
B. CURRENT MITIGATION ACTIVITIES : PREVENTION
C. FUTURE MITIGATION ACTIVITIES : REMOVAL
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 29
Prevention activities Effectiveness
1- Limitation of debris release during operations Low
2- Minimization of potential fragmentation during operations Low
3- Limitation of the probability of accidental collision High
4- Avoidance of intentional destruction and other harmful activities Medium
5- Minimization of potential post-mission fragmentations Medium
6- Limitation of abandoned spacecraft and launchers in the LEO region Medium
Source: IADC and : Space Debris, Team Project Report, ISU SSP 2012
B.1 – Current Mitigation Activities: Prevention
2. REVIEW ON SPACE DEBRIS ACTIVITIES
Collisions between debris are not included !
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 30
B.1 – Space Debris Simulator
2. REVIEW ON SPACE DEBRIS ACTIVITIES
Source: Raytheon versus Lockheed Contract
$3.5 billion Air Force contract
Goal : Track 20k to 200k space debris !
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 31
2. REVIEW ON SPACE DEBRIS ACTIVITIES
B.2 – Current Mitigation Activities and Limitations
IADC is no ‘real’ authority to bind internationally space debris guidelines:
• There is no mention concerning military activities in space (only for civil)
• No Space Authority !
Space debris activities are only dedicated to reduce new debris production
• These activities lack of active removal actions.
Current Outer Space laws are inadequate because of
• Significant distrust between space applicants (countries, military, industrial spying, etc.)
• No approved protocol
• Liability Convention terms are imprecise (Significant treat only)
• United States ITAR regulations are complicating international collaboration in space
development
Space debris mitigations are a necessary but insufficient
• it must be accompanied by space debris environment remediation.
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 32
2. REVIEW ON SPACE DEBRIS ACTIVITIES
A. SPACE DEBRIS PROGRAMS
B. CURRENT MITIGATION ACTIVITIES : PREVENTION
C. FUTURE MITIGATION PROJECTS: REMOVAL
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 33
Source: Space Debris, Team Project Report, ISU SSP 2012
Debris Deorbiting Activities :
• Instant propulsive method
• Deferred propulsive method
• Non-propulsive method
Debris Capture Activities :
• Capture methods only
C.1 – Different Approaches for Debris Removal
2. REVIEW ON SPACE DEBRIS ACTIVITIES
Orion Project, Nasa
Breaking Sail, ESA
CleanSpace, ESA
Phoenix, DARPA
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 34
Source: Space Debris, Team Project Report, ISU SSP 2012
C.2 – Debris Removal: options
2. REVIEW ON SPACE DEBRIS ACTIVITIES
Options / Projects Deorbiting Capture Debris target
Electromagnetic tethers √ Medium debris
Balloons √ Large debris
Solar sails √ Small debris
Propulsion engines √ Large debris
Lasers beams √ Large debris
Nets √ Small debris
Sweepers √ Small debris
Robotic arms √ √ Large debris
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 35
3. REVIEW OF SPACE VEHICLE TECHNOLOGIES
A.1 – Manned and Unmanned Space Vehicles
A.2 – Advantages of UAV (Unmanned Aerial Vehicle)
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 36
3. REVIEW OF SPACE VEHICLE TECHNOLOGIES
Source: NASA , Astronautix and image from StyleofSpeed
Lockheed Martin : X-33 Project
Project started : 1996 Official end : 2001 (US DoD)
Manned and unmanned rocket plane
Sub-scale advanced technology demonstrator
Increase launch vehicle safety, reliability and reduce cost
payload into space (from $10,000 to $1,000).
Program canceled (2009) : flight instability and excess weight
A.1 – Manned and Unmanned Space Vehicles
THE X-33 SPECIFICATIONS
Length: 69 feet
Wingspan: 77 feet
Weight: 210,000 lbs.
Volume: 565 feet3
Altitude: Suborbital
Category: SSTO
Potential Crew: 7
Official designation : Venture Star Launch Vehicle 3
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 37
3. REVIEW OF SPACE VEHICLE TECHNOLOGIES
Virgin SPACESHIP-TWO
Manned and suborbital
10 Oct 2010 (first glide flight) and 29 April 2013 (first powered flight)
Space plane designed primarily for commercial space tourism
Can also carry onboard scientific payloads for NASA and other organizations.
Initial ticket price of US$200,000. Beginning planned for 2014 !
Source: VIRGINGALACTIC and WIKIPEDIA
A.1 – Manned and Unmanned Space Vehicles
THE SPACESHIPTWO SPECIFICATIONS
Length: 60 feet
Diameter: 90 inches
Altitude: Suborbital
Category: SSTO
Crew: 2
Passengers: 6
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 38
Source: NASA and UNIVERSE TODAY
DREAM CHASER
Reusable composite spacecraft: Manned, suborbital and orbital
Transport astronauts to Low Earth Orbit (LEO) destinations, such as the International Space
Station (ISS)
Aerial testes planned throughout 2013
Vertical-takeoff, horizontal-landing (VTHL)
Potential orbital space tourism
THE DREAM CHASER HIGHLIGHTS
Length: 29.5 feet
Wingspan: 22.9 feet
Volume: 565 feet3
Crew: 7
3. REVIEW OF SPACE VEHICLES TECHNOLOGIES
A.1 – Manned and Unmanned Space Vehicles
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 39
Source: SPACE-X
SPACE-X DRAGON
Manned and robotic operation, orbital (with rocket, TSTO), fully commercial
In 2012, it became the first commercial spacecraft (unmanned) to deliver cargo
to the ISS (In: 460 kg food and clothing and out : 620 kg of cargo to Earth)
Reusable spacecraft to deliver crew and cargo to orbiting destinations
NASA awards Space-X $440M to aid development of crew capability
THE DRAGON HIGHLIGHTS
Diameter: 12 feet
Wingspan: 14.1 feet
Height: 23.6 feet
Crew: 0 to 7
Total payload: 13,228 lbs
Orbit duration 2 years
3. REVIEW OF SPACE VEHICLES TECHNOLOGIES
A.1 – Manned and Unmanned Space Vehicles
Falcon 9 v1.0
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 40
3. REVIEW OF SPACE VEHICLE TECHNOLOGIES
Source: BOEING and Wikipedia
Controversy:
260 days in space in
2012 following
Chinese Satellite !
A.1 – Manned and Unmanned Space Vehicles
BOEING X-37B
Unmanned, orbital, re-entry spacecraft operating at LEO
First spaceflight in 2006 2 units owned by USAF
Advanced technology demonstrator for unmanned and re-entry capabilities
In 2011, X-37C scale-up variant (larger)
THE BOEING X-37B FACTS
Length: 29.3 feet
Wingspan: 14.1 feet
Height: 9.6 feet
Category: SSTO
Crew: Remotely controlled from ground
Propulsion: Rocketdyne AR2-3 rocket engines
Max. thrust: 11,000 lbs.
Max. Speed: 28,000 mph
Cruise speed: 17,500 mph
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 41
3. REVIEW OF SPACE VEHICLE TECHNOLOGIES
Source: Skylon Space Plane and Wikipedia
A.1 – Manned and Unmanned Space Vehicles
SKYLON
Unmanned, orbital, re-usable spacecraft operating at LEO
Spaceflight to be designed by Reaction Engines Limited (UK)
Program projected to cost $12 billion
To deliver payload in orbit
First test flights expected in 2019
THE SKYLON FACTS
Length: 273 feet
Wingspan: 82 feet
Category: SSTO
Crew: none, remote controlled from ground
Capacity: 30 passengers
Propulsion: SABRE engine
Max. cargo: 760,000 lbs.
Max. Speed: Mach 5.5
Max. altitude: 300 km
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 42
3. REVIEW OF SPACE VEHICLE TECHNOLOGIES
Deutsche Orbital Servicing Mission (DEOS)
Objective: capture errant satellites using an experimental servicing
satellite
Space vehicle: free-flying space robot
Contract: €15M awarded to Astrium GmbH (September 13, 2012)
Missions: deorbiting, space debris removal, complex assembly
assistance functions, maintenance and repair.
Source: SPACETECH-i , SPACE SAFETY MAGAZINE and DLR Robotic Technologies
A.1 – Manned and Unmanned Space Vehicles
First On-Orbit Servicing Satellite !
Beginning of new concept in Satellite design !
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 43
3. REVIEW OF SPACE VEHICLE TECHNOLOGIES
LYNX Mark Series
The Lynx is intended to space tourism (started in 2008)
Suborbital horizontal-takeoff, horizontal-landing
It will operate as an FAA AST-licensed suborbital,
reusable, launch vehicle under visual flight rules (VFR).
Designed for 40 flight before preventive maintenance.
175 Lynx Flight presold ticket to Space @ 95kUSD
Source: XCOR
A.1 – Manned and Unmanned Space Vehicles
THE LYNX MK2 FACTS
Length: 27.9 feet
Wingspan: 24.0 feet
Height: 7.22 feet
Category: SSTO
Crew: 2 (incl. pilot)
Propulsion: Rocket engines
Max. thrust: 11,600 lbs
Reusable. Reliable. Cost Effective
The Lynx Mark III
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 44
Mission features Manned
Vehicle
Satellite
Vehicle UAV
1- Quick Time to Mission Execution X X
2- Fast turnaround between Missions X X
3- Suborbital flights
4- High tempo operations: more missions per day X X
5- Horizontal takeoff – horizontal landing X
6- Safety for crew X
7- Reliable
8- Reusable X
B.1 – Advantages of UAV (Part I): MISSION ASPECTS
3. REVIEW OF SPACE VEHICLES TECHNOLOGIES
UAV-SSS Concept : Save Life, Save Money and Save Time
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 45
Financial features Manned
Vehicle
Satellite
Vehicle
UAV
Low cost operations and maintenance X X
Low crew expenses X X
Easier to launch X
Easier to replace X X
Easier to repair X X
More flights X X
Durable missions (least training period for crew) X X
3. REVIEW OF SPACE VEHICLES TECHNOLOGIES
B.2 – Advantages of UAV (Part II): FINANCIAL ASPECTS
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 46
Medical concerns Manned
Vehicle
Satellite
Vehicle UAV
Astronauts can experience immune deficiency Yes Yes None
Astronauts can experience collapse bone and tissue Yes Yes None
Astronauts can experience sickness Yes Yes None
Astronauts can experience radiation poisoning Yes Yes None
Astronauts can lead to injuries or fatalities Yes Yes None
B.3 – Advantages of UAV (Part III): HUMAN FACTORS
3. REVIEW OF SPACE VEHICLES TECHNOLOGIES
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 47
4. GLANCE ON AMOOS PROJECT
Team Project of ISU-SSP 2014
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 48
Mission of a virtual scenario to repair
an important satellite in LEO
4. GLANCE ON ISU-SSP 2014 AMOOS PROJECT
4.1 – AMOOS Mission Planning
1.
Analysis
2.
Design
3.
Preparation
4.
Execution
5.
Post-analysis
ISU-SSP 2014 PROJECT :
Analyse, develop, and realize a virtual scenario in which a critical satellite subsystem faulty operation
has already been detected and on the need to repair this important LEO satellite autonomously on-orbit.
THEORICAL PRACTICAL
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 49
4.2 – AMOOS Challenges, Assignments and Deliverables
The Team Project must:
4. GLANCE ON ISU-SSP 2014 AMOOS PROJECT
1. Undertake technical analysis on potential key technologies (Canadian and International).
• UAV, Robotic Arm, Satellite, Mission.
2. Describe legal and political protocols, agreements and recommendations (Legal Plan).
3. Assess economic feasibility of AMOOS project (Business Plan).
4. Propose new satellite design Concept (Modularity) for On-Orbit Servicing
5. Undertake potential threats and risks on unmanned mission to space.
6. Analyse and Execute AMOOS Mission (Planning, coordination, execution).
7. Post-Mission Analysis and Recommendations
DELIVERABLES : Report + Virtual Mission Execution (Recorded Video)
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 50
4.3 – Interdisciplinary scope
The Project is expected to promote:
Engineering
Process
Business
Model
International
Policies & laws
Satellite
Applications
Space & Society
issues
Life & Physical
Sciences
4. GLANCE ON ISU-SSP 2014 AMOOS PROJECT
Team of about
~30 ISU Students
AMOOS Project
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 51
Source: Image taken from XCOR GALLERY
Target: LEO defective satellite (TBD)
Control center: LASSENA Ground Controlled Station
Spacecraft: UAV Version of LYNX MARK III
Destination: Low Earth Orbit (LEO) at 700km
Mission: On-orbit servicing (refuel, repair, replacement)
MISSION :
1. Horizontal takeoff from runway
2. Autonomous navigation to orbital destination
3. Rendezvous with the defective satellite
4. Docking / berthing
5. On-board robotics for satellite defect repair
6. Return navigation mission
7. Safe horizontal flight landing
4. GLANCE ON ISU-SSP 2014 AMOOS PROJECT
4.4 – AMOOS Mission Scenario
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 52
ÉTS based Marinvent Corporation
Flight Research Simulator
(used as UAV Lynx Ground Control
Simulator)
ÉTS UAV Ground Control
Operation Center (Mission
section)
4.5 – AMOOS Mission Control Center and Facilities
ÉTS UAV Ground Control
Operation Center
(Planning section)
4. GLANCE ON ISU-SSP 2014 AMOOS PROJECT
ÉTS SatCom facilities LASSENA Team and Facilities
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 53
4. GLANCE ON ISU-SSP 2014 AMOOS PROJECT
4.5 – Presentation of X-Plane 10
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 54
4. GLANCE ON ISU-SSP 2014 AMOOS PROJECT
4.5 – Presentation of STK 10 AGI Software
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 55
4. GLANCE ON ISU-SSP 2014 AMOOS PROJECT
4.5 – Real UAV/Drone Simulation
• Fully controlled by the ÉTS Simulator
• Indoor usage for Mission Planning
• Outdoor usage for Mission Execution
Subscale Demonstration of Real AMOOS Trajectory
300’
200’ UAV
Defective
Satellite
Rendezvous and Servicing !
Remotely
controlled
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 56
Source: Canada Space Agency and The Next-Generation Canadarm
TECHNOLOGY STATUS OF CANADARM (SRMS)
Shuttle Remote Manipulator System (SRMS)
Complex operations handling
Precise capture of objects
Range of motion larger than human arm.
Length: 58 feet.
Weight: 3968 lbs.
Thickness: 1.15 feet.
Degrees of freedom: 7 (shoulder: 3, elbow: 1, wrist: 1).
Cameras: 4
Lift: 116 tons in space.
4. GLANCE ON ISU-SSP 2014 AMOOS PROJECT
4.6 – The Next-Generation Small Canadarm
In potential
collaboration with :
Visit of the CSA and CANADARM Simulator
+ Expert Conferences …
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 57
5. CONCLUSION
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 58
5.1 – In Summary
5. CONCLUSION
1. A technological challenge
2. An urgent need to reduce the proliferation of Space Debris
3. A commercially viable solution to extend Satellite Life
4. An innovative idea gaining popularity
5. A real solution providing long term maintenance
6. A safe and cost effective solution for space operations
7. A need for Space Innovation
The AMOOS is :
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 59
For Satellites Maintenance:
1. Add robustness to satellite subsystems
2. Extend satellite lifetime
3. Increase satellite performances
4. Recycle and re-use satellite parts
5. Reduce total operational costs
On Space Debris:
1. Reduce overall risks to space crew
2. Reduce Space Debris threats and proliferation
3. Allow execution of space debris removal technologies
5.2 – Advantages of AMOOS over traditional approaches
5. CONCLUSION
Many other outcomes :
1. To put payload in
space
2. To allow Canada
sovereignty in Space !
3. etc.
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 60
5.3 – Potential opportunities
5. CONCLUSION
For Unmanned Mission to Space
… Participate in efforts for unmanned space exploration.
… Participate in efforts for robotic space missions.
… Participates in efforts for civil use of UAV in Space.
For Space Debris Issues
… Participate in efforts to reduce orbital junk.
… Participate in efforts to reduce orbital mission threats.
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 61
5.4 – Potential opportunities
5. CONCLUSION
For Canada Space Industry
… Participate in efforts for space business in commercial applications.
… Participate in efforts for international cooperation for space management, policies and laws.
… Provide new services for customers.
… Reinforce Canada national sovereignty.
… Participate in the next-generation of Canada Space Technologies.
… Huge potential of national R&D projects and programs.
… Economically viable for Canada Space industries.
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 62
5.5 – Potential Canadian Support and Partnership
5. CONCLUSION
Numerous potential industries :
Governmental organizations :
Etc.
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 63
5. CONCLUSION
5.1 – Virtual Scenario of AMOOS Mission
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 64
ISU – SSP 2014 Evening
René Jr. Landry
18 September 2013
International Space University – Team Project Proposal
Laboratoire Spécialisé en Systèmes Embarqués, Navigation et Avionique
www.lassena.etsmtl.ca
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 65
ISU – SSP 2014 Evening
Alexis Do Sanou
PhD Candidate at LASSENA
www.lassena.etsmtl.ca
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 66
APPENDIX 1:
DATA MINIG ON PREVIOUS ISU PROJECTS REPORTS
Year SSP MSS TOTAL
2013 1 1
2012 5 2 7
2011 3 2 5
2010 3 2 5
2009 2 2 4
2008 3 2 5
2007 4 2 6
2006 3 2 5
2005 3 2 5
2004 3 2 5
2003 3 2 5
2002 2 2 4
2001 2 2 4
Year SSP MSS TOTAL
2000 3 1 4
1999 2 1 3
1998 2 1 3
1997 3 1 4
1996 2 1 3
1995 2 2
1994 2 2
1993 1 1
1992 2 2
1991 1 1
1990 2 2
1989 2 2
1988 1 1
Total SSP: 62 Total MSS: 29 Total TP: 91 Studies on space debris: 3 (2003 – 2007 – 2012) OOS: 1 (2007)
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5.4 – Canada sovereignty
Project goal :
To develop a Canadian Launcher
Investigators :
DRDC (Defence Research and Development Canada) and CSA
Project proposed name :
Microsatellite Launcher Critical Technologies R&D Canada
Status:
Still in study at CSA !
APPENDIX 2:
CANADIAN MICROSATELLITE LAUNCHER
Example of project financed by DRDC : Canadian Small Launch Vehicle Guidance, Navigation and Control Concept Design and Analysis
AMOOS Project
may be an
opportunity to join !
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 68
5.4 – Example of another expertise in Canada
APPENDIX 3:
MULTI-FUEL DASS ENGINE APPLICATIONS
http://www.spaceenginesystems.com
Multi-fuel DASS Engine Applications
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APPENDIX 4:
SPACE JUNK 3D
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 70
REFERENCES (LINKS RELATED IN THIS DOCUMENT)
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I A D C : h t t p : / / w w w . i a d c - o n l i n e . o r g /
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X - 3 3 : h t t p : / / w w w . n a s a . g o v / c e n t e r s / m a r s h a l l / n e w s / b a c k g r o u n d / f a c t s / x 3 3 . h t m l
V I R G I N : h t t p : / / w w w . v i r g i n g a l a c t i c . c o m / o v e r v i e w / s p a c e s h i p s /
C H A S E R : h t t p : / / w w w . u n i v e r s e t o d a y . c o m / 1 0 2 0 2 0 / s i e r r a - n e v a d a - d r e a m - c h a s e r - g e t s - w i n g s - a n d - t a i l - s t a r t s - g r o u n d - t e s t i n g /
C H A S E R : h t t p : / / w w w . n a s a s p a c e f l i g h t . c o m / 2 0 1 3 / 0 7 / d r e a m - c h a s e r - o p e n i n g - t o w - t e s t s - d r y d e n /
S P A C E - X : h t t p : / / w w w . s p a c e x . c o m / d r a g o n . p h p
X - 3 7 : h t t p : / / w w w . b o e i n g . c o m / a d v e r t i s i n g / s p a c e / a d v a n c e d s y s t e m s / x 3 7 . h t m l
S K Y L O N : h t t p : / / d e s i g n y o u t r u s t . c o m / t e c h n o l o g y / s k y l o n - s p a c e - p l a n e /
S K Y L O N : h t t p : / / e n . w i k i p e d i a . o r g / w i k i / S k y l o n _ ( s p a c e c r a f t )
X C O R : h t t p : / / w w w . x c o r . c o m / l y n x p a y l o a d s / i n d e x . h t m l
D E O S : h t t p : / / w w w . s p a c e t e c h - i . c o m / d e u t s c h e - o r b i t a l e - s e r v i c i n g - m i s s i o n . h t m l
C S A C a n a d a r m : h t t p : / / w w w . a s c - c s a . g c . c a /
X - P l a n e : h t t p : / / w w w . x - p l a n e . c o m / d e s k t o p / h o m e /
S T K : h t t p : / / w w w . a g i . c o m / p r o d u c t s / s t k / m o d u l e s / d e f a u l t . a s p x / i d / s t k - f r e e
I S U : h t t p : / / i s u l i b r a r y . i s u n e t . e d u / o p a c /
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 71
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M u n i c h G e r m a n y . i - S A I R A S 2 0 1 0 , S a p p o r o , J a p a n . S p a c e T e c h P o s t - G r a d u a t e M a s t e r P r o g r a m o n S p a c e S y s t e m s a n d B u s i n e s s
E n g i n e e r i n g b y D e l f t U n i v e r s i t y . 8 p .
1 1 . S é n é c h a l , T h i e r r y . X X X X . « S p a c e D e b r i s P o l l u t i o n : A C o n v e n t i o n P r o p o s a l » . p p 3 9 - 6 5 .
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I n t e r n a t i o n a l A c a d e m e y o f A s t r o n a u t i c s ( I A A ) , P a r i s ( F r a n c e ) . S P - 1 3 0 1 . 6 3 p .
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ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 73
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E n v i r o n m e n t » . 1 6 p .
3 2 . A i r F o r c e S p a c e C o m m a n d . 2 0 1 0 . « E n d - o f - L i f e d i s p o s a l o f S a t e l l i t e s i n L o w - E a r t h O r b i t » . S p a c e a n d M i s s i l e S y s t e m s C e n t e r
S t a n d a r d ( S M C - S - 0 2 2 ) . 4 7 p .
ISU SSP 2014 | Team Project Proposal | AMOOS Project 19/09/2013 74
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3 3 . R u s t i e L . H i b b a r d . 1 9 9 6 . « S a t e l l i t e O n - O r b i t R e f u e l l i n g : A C o s t E f f e c t i v e n e s s A n a l y s i s » . T h e s i s : N a v a l P o s t g r a d u a t e S c h o o l . 9 9
p .
3 4 . J o s h R e d d i n g a n d K e l l y J . H a y h u r s t . 2 0 1 3 . « G N S S & U n m a n n e d A e r i a l S y s t e m s : T h e R o a d A h e a d » . I n s i d e G N S S M a g a z i n e . 5 7 p .
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