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ISIS – Innovative Solutions In Space
Company Presentation
ISIS group - overview
• Founded in 2006, spin-off from Delfi-C3 project
• Currently about 50 staff (FTE)
• Provider of small satellite products and services
• Vertically integrated small satellite company
• Offices in Delft, The Netherlands and Somerset West, South Africa
• 2013 highlights:
– Triton-1 Satellite for SAT-AIS successfully launched
– Responsible for launch 11% of all satellites in 2013
– Record sales to 6 continents
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0
10
20
30
40
50
60
2007 2008 2009 2010 2011 2012 2013 2014
No. of Employees
People at ISIS • 50 FTE
• 45% international
– 20 Nationalities
– 12+ languages
Vocational
Beng / BSc
MSc
PhD
0% 10% 20% 30% 40% 50% 60% 70%
< 25
25-35
35-45
45-55
55-65
> 65
Age of Employees
Internationally active
Capabilities and competencies
Systems Engineering
MAIV Expertise
Radio Frequency Engineering
Electrical Engineering
Attitude Control Engineering
Mechanical Engineering
Embedded Software
Flight Software Engineering
Main Activities
Products • CubeSat Avionics
– Radios
– Antennas
– Solar Arrays
– OBCs
– Etc.
• Ground Stations
• Operations Centers
• Support equipment
• Software Tools
• Both standardized and custom developments
Launches • Launch Services
– DNEPR
– Soyuz
– Long March
– VEGA
– ANTARES
– Falcon-9
– PSLV
• Piggy back – CubeSats
– Nanosats
– Microsats
• Associated Services – Testing
– Insurance
Missions • Turn key solutions
– CubeSat platforms
– Payloads
– Ground segment
– Launch
– Operations
• Fast implementation times
• Including training, knowledge transfer and co-development
Applications • Based on satellite
networks – Radio Astronomy
– Maritime Monitoring
– Agriculture
– Communications
• Global Coverage
• High revisit times
• Fully integrated solutions
Nanosatellite Products
ISIlaunch Launch Services
DNEPR – November 2013
June ‘14 – DNEPR – 23 satellites
3/5/2015 11
ISIS 2-Unit CubeSat Platform First CubeSat Mission Capability
Platform Specifications
Mass: 2 -3 kg
Power: 5W peak, 3W AOP
Downlink: 10 kbps
Pointing knowledge: < 5°
Pointing Accurary: <10 °
Orbit determination: -
Propulsion: -
Payload Accommodation
Mass: 1 kg
Power: 4W peak, 1,5W AOP
Data Storage: > 2 Gbit
Possible Payloads
Small camera
Technology demonstrator
Space Weather
Launch Options
Dispenser: ISIPOD
Lowest Cost
For Small Experiments Limited data downlink
ISIS 3-Unit CubeSat Platform Low cost operational missions
Platform Specifications
Total mass: 4 kg
Power: 20W peak, 10W AOP
Downlink: 100-1000 kbps
Pointing knowledge: < 0.1°
Pointing Accurary: <1.0 °
Orbit determination: GPS
Propulsion: -
Payload Accommodation
Mass: 1-2 kg
Power: 20W peak, 10W AOP
Data Storage: > 20Gbit
Possible Payloads
SAT-AIS receiver
Science payload
Mid-resolution imagers
Launch Options
Dispenser: 3U ISIPOD / QP
More capable platform
Small operarational payloads
More Power for payloads
ISIS 12-Unit CubeSat Platform Operational remote sensing mission
Platform Specifications
Mass: 15-20 kg
Power: 25W peak, 15W AOP
Downlink: 1-10 Mbps
Pointing knowledge: < 0.05°
Pointing Accurary: <0,2 °
Orbit determination: GPS
Propulsion: Optional
Payload Accommodation
Mass: 5-10 kg
Power: 20W peak, 10W AOP
Data Storage: > 100 Gbit
Possible Payloads
Thermal Infrared Imager
Multispectral imagers
Science payload
Mid-resolution imagers
Launch Options
Dispenser: 12U Quadpack
Larger volume allows redundant chains
Higher data rates More Capable payloads
3/5/2015 15
Vessel tracking issue: • Near shore only • Limited coverage • Cooperating vessels
Growing need: • Cargo Owners • Supply chain • Logistics • Monitoring • Enforcement • Services • Safety
Problem: Vessel wherabouts
Applicable to : • 100,000+ large vessels (>300GT) • % of the 4,000,000+ fishing vessels
16
IDS – Ocean Traffic Monitoring
TRITON Network
“Providing near-realtime position, heading and vessel information of every shipping vessel in the world using a collaborative
network of small satellites”
17
Other Applications for Nanosats
• Global Coverage – Oceans, etc – Including arctic – Required Infrastructure Independence
• Improved Temporal Resolution
– Augmenting existing infrastructure – Regular mapping or monitoring
• Improved Responsiveness – Fast deployment – Rapid replenishment
Education & outreach
• CanSat Competition
– In NL since 2007
– ISIS coordinator
– Aimed at High Schools
• Support Space Education
– High Schools
– Universities
• Leiden
• Delft
– Guest Lectures
• Various intern. universities
• Formal Training Programme
– DLR
– Universities
• Hands-on Training solutions
• Integrated programmes
– Training
– Building satellites
– Knowledge transfer
ISIS CubeSat Training Program
1. Hands-on training and courses
2. Set up of local development lab
3. Multi-satellite program
1. Buy one and assist in assembly
2. Assemble one and assist in design
3. Develop one, with assistance from ISIS
4. Scaleable to needs
Cubesat Training Programme Multiple training modules available for up to 10 participants
Space Systems Engineering
• 4 day course in Delft
• € 15,000
Mission and Satellite Design
• 4 day course in Delft
• € 15,000
EyaSat training
• 3 day course in Delft
• 2 x EyaSAT training kits
• € 25,000
CubeSat Training
• 4 day course in Delft
• 1 x CubeSat Training Kit
• € 65,000
On request
• ADCS design
• Flight Software design
• Verification
• Assembly & integration
• Operations
Establishment of CubeSat development lab ISIS to provide a CubeSat Development lab at customer location
CubeSat Development Kit
• EM CubeSat & GSE
• 2nd EPS and OBC
• € 55,000
Simulators and SW tools
• ADCS simulator
• Power simulator
• € 25,000
Support Equipment
• Jigs and supports
• Interfacing equipment
• € 15,000
Nanosat Ground Station
• UHF/VHF/S-band
• Onsite installation
• € 60,000
On request
• Lab furniture
• Lab equipment
• Cleanrooms
• Test facilities
• Mission control
3 Stage Nanosatellite Programme
Multiple satellites in orbit
• 3-satellites
• 4 year program
Increasing Involvement
• Learning / Observing
• Active participation
• In control of the program
Continuing Support
• Review support
• Design support
• MAIV support
• Operations support
Scaleable and modular
• Tailored to specific needs
• Test facilities
Stage-1: Satellite Procurement For the first steps into space and to learn from experienced CubeSat builders
Platform Specifications
Total mass: 1 kg
Power: 2W peak, 1W AOP
Downlink: 1.2 – 9.6 kbps
Pointing knowledge: < 5°
Pointing Accurary: <10.0 °
Orbit determination: No
Propulsion: No
Cost: 75-150 k€
Payload Accommodation
Mass: 100-200 g
Power: 1W peak, 0.5W AOP
Data Storage: > 4 Gbit
Possible Payloads
Amateur Payloads
Technology Demonstratoion
Launch Options
Dispenser: ISIPOD
Cost: 60-80 k€
Stage-2: Configuration and Integration Full participation in relatization of space mission
Platform Specifications
Total mass: 2 kg
Power: 5W peak, 3W AOP
Downlink: 1.2 – 9.6 kbps
Pointing knowledge: < 5°
Pointing Accurary: <10.0 °
Orbit determination: No
Propulsion: No
Cost: 200-350 k€
Payload Accommodation
Mass: 500-750 g
Power: 1W peak, 0.5W AOP
Data Storage: > 4 Gbit
Possible Payloads
Amateur Payloads
Technology Demonstratoion
Launch Options
Dispenser: ISIPOD
Cost: 110 - 130 k€
Stage 3: Full National Development ISIS provides design support, hardware buidling blocks and launch service
Platform Specifications
Total mass: 3 kg
Power: 7W peak, 4W AOP
Downlink: 10-100 kbps
Pointing knowledge: < 1°
Pointing Accurary: <5.0 °
Orbit determination: No
Propulsion: No
Cost: 250-500 k€
Payload Accommodation
Mass: 1 – 1,5 k g
Power: 5W peak, 2.5W AOP
Data Storage: > 4 Gbit
Possible Payloads
Amateur Payloads
Technology Demonstratoion
Launch Options
Dispenser: ISIPOD
Cost: ~200 k€
Thank you for your attention! Jeroen Rotteveel - [email protected] - 003 1 15 256 9018
ISIS Contact information:
Molengraaffsingel 12-14,
2629 JD Delft,
The Netherlands
Tel: +31 15 256 9018
Email: [email protected]
Web: www.isispace.nl
