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Building Low Cost Cubesat: Guidelines and Design Approach Ibtissam Latachi PPR / 2015 /12 4 th IAA Conference on University Satellite Missions and Cubesat Workshop IAA-AAS-CU-17-06-02

Building Low Cost Cubesat - GAUSS Srl · 2018. 2. 14. · Introduction - Why Cubesats? • The Cubesat model provides almost all of the benefits of a larger program at a fraction

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Page 1: Building Low Cost Cubesat - GAUSS Srl · 2018. 2. 14. · Introduction - Why Cubesats? • The Cubesat model provides almost all of the benefits of a larger program at a fraction

Building Low Cost Cubesat: Guidelines and Design Approach

Ibtissam Latachi

PPR / 2015 /12

4th IAA Conference on University Satellite Missions and

Cubesat WorkshopIAA-AAS-CU-17-06-02

Page 2: Building Low Cost Cubesat - GAUSS Srl · 2018. 2. 14. · Introduction - Why Cubesats? • The Cubesat model provides almost all of the benefits of a larger program at a fraction

PLAN

Introduction

Methodology

Mission Analysis Processes

System Engineering Processes

Platform: Available Options and Trade-offs

Management Processes

Conclusion & Futur Perspectives

Page 3: Building Low Cost Cubesat - GAUSS Srl · 2018. 2. 14. · Introduction - Why Cubesats? • The Cubesat model provides almost all of the benefits of a larger program at a fraction

Introduction - Why Cubesats?

• The Cubesat model provides almost all of the benefits

of a larger program at a fraction cost.

• Cubesats are valuable educational tool to leverage

aerospace capacity building since emphasis is

put on the “learn-by-doing” process.

4th IAA Conference on University Satellite Missions and Cubesat Workshop

Page 4: Building Low Cost Cubesat - GAUSS Srl · 2018. 2. 14. · Introduction - Why Cubesats? • The Cubesat model provides almost all of the benefits of a larger program at a fraction

Introduction –MASAT 1Objectives:

1. Enhance capacity building in

space technology and

spacecraft engineering

through designing and

integration of both the space

and ground segment

2. Establish a reliable radio link

with low-cost mission

control ground station for

control, command, and

telemetry retrieval.

3. On-orbit reconfiguration and

testing of the FPGA based

secondary OBC.

4th IAA Conference on University Satellite Missions and Cubesat Workshop

Page 5: Building Low Cost Cubesat - GAUSS Srl · 2018. 2. 14. · Introduction - Why Cubesats? • The Cubesat model provides almost all of the benefits of a larger program at a fraction

Methodology –ECSS Framework -

4th IAA Conference on University Satellite Missions and Cubesat Workshop

Page 6: Building Low Cost Cubesat - GAUSS Srl · 2018. 2. 14. · Introduction - Why Cubesats? • The Cubesat model provides almost all of the benefits of a larger program at a fraction

Methodology - Approach –

Concurrent System Engineering

Approach

Iterative: to cope with eventual requirements

changes and all the discrepancies which may arise

during the design process,

Recursive: to design next lower layer subsystems

or to realize next upper layer elements within the

system structure

4th IAA Conference on University Satellite Missions and Cubesat Workshop

Page 7: Building Low Cost Cubesat - GAUSS Srl · 2018. 2. 14. · Introduction - Why Cubesats? • The Cubesat model provides almost all of the benefits of a larger program at a fraction

Mission Analysis Process

4th IAA Conference on University Satellite Missions and Cubesat Workshop

Page 8: Building Low Cost Cubesat - GAUSS Srl · 2018. 2. 14. · Introduction - Why Cubesats? • The Cubesat model provides almost all of the benefits of a larger program at a fraction

System Engineering Processes

4th IAA Conference on University Satellite Missions and Cubesat Workshop

Page 9: Building Low Cost Cubesat - GAUSS Srl · 2018. 2. 14. · Introduction - Why Cubesats? • The Cubesat model provides almost all of the benefits of a larger program at a fraction

Platform: Structure and SC configuration

Structure Satellite configuration

Physical configuration:

Layers / Slots

Logical configuration:

Centered / Distributed

4th IAA Conference on University Satellite Missions and Cubesat Workshop

Mass budget:

The CDS standard limits the mass of

the Cubesat to a maximum of 1.4 kg

with a security margin of 10%.

Page 10: Building Low Cost Cubesat - GAUSS Srl · 2018. 2. 14. · Introduction - Why Cubesats? • The Cubesat model provides almost all of the benefits of a larger program at a fraction

Platform: Attitude Control

Passive attitude control:

+ No energy consumption

+ No dedicated card slot

+ Easy configuration

- No pointing accuracy

4th IAA Conference on University Satellite Missions and Cubesat Workshop

Page 11: Building Low Cost Cubesat - GAUSS Srl · 2018. 2. 14. · Introduction - Why Cubesats? • The Cubesat model provides almost all of the benefits of a larger program at a fraction

Platform: CommunicationSpace segment Ground segment

4th IAA Conference on University Satellite Missions and Cubesat Workshop

Communication system parameters:

Transmitted Power , Gains , Noise

Temperature

Page 12: Building Low Cost Cubesat - GAUSS Srl · 2018. 2. 14. · Introduction - Why Cubesats? • The Cubesat model provides almost all of the benefits of a larger program at a fraction

Platform: Communication

4th IAA Conference on University Satellite Missions and Cubesat Workshop

Choice criteria:

Power efficiency

Bandwidth efficiency

Page 13: Building Low Cost Cubesat - GAUSS Srl · 2018. 2. 14. · Introduction - Why Cubesats? • The Cubesat model provides almost all of the benefits of a larger program at a fraction

Platform: Communication

4th IAA Conference on University Satellite Missions and Cubesat Workshop

Link Budget Analysis

Page 14: Building Low Cost Cubesat - GAUSS Srl · 2018. 2. 14. · Introduction - Why Cubesats? • The Cubesat model provides almost all of the benefits of a larger program at a fraction

Platform: On-board Data Handling

4th IAA Conference on University Satellite Missions and Cubesat Workshop

choice criteria are: Resilience against the harsh space environment,

High processing power,

Power consumption and memory storage.

Flight heritage to ensure reliability,

Hardware or software redundancy to minimize single point of failures,

Price,

Page 15: Building Low Cost Cubesat - GAUSS Srl · 2018. 2. 14. · Introduction - Why Cubesats? • The Cubesat model provides almost all of the benefits of a larger program at a fraction

Platform: On-board Energy

4th IAA Conference on University Satellite Missions and Cubesat Workshop

Solar panels:

• Body mounted /deployed

• Simple/ double / triple junctions

Batteries: Low DOD (Depth of Discharge) is recommended for

better resistance to radiations, better temperature coefficients, higher levels of delivered power, and hence higher efficiency.

Page 16: Building Low Cost Cubesat - GAUSS Srl · 2018. 2. 14. · Introduction - Why Cubesats? • The Cubesat model provides almost all of the benefits of a larger program at a fraction

Platform: On-board Energy

4th IAA Conference on University Satellite Missions and Cubesat Workshop

Power Budget Analysis

Page 17: Building Low Cost Cubesat - GAUSS Srl · 2018. 2. 14. · Introduction - Why Cubesats? • The Cubesat model provides almost all of the benefits of a larger program at a fraction

Production and Qualification Processes

Activities:

• Implementation approach : Fabricate/ procure/ reuse hardware and

code software.

• Prototype/ protoflight verification, validation and integration

• Run qualification tests such as : vibration, static, mechanisms,

thermal vacuum tests

• Run final functional tests

• Packaging

4th IAA Conference on University Satellite Missions and Cubesat Workshop

Page 18: Building Low Cost Cubesat - GAUSS Srl · 2018. 2. 14. · Introduction - Why Cubesats? • The Cubesat model provides almost all of the benefits of a larger program at a fraction

Management Processes

4th IAA Conference on University Satellite Missions and Cubesat Workshop

Project Management

Project organization and planning

* Definition of stackeholders

* Definition of project life cycle and milestones

Mission architecture definition

* Definition of the payloads,

* Identification of potential launch vehicles, constraints and proposed services,

* Identification of the space segment configuration

* Identification of the ground segment locations

* Definition of communication link configuration, frequency bands and transmission mode and frequency allocation license

* Product Tree and Work breakdown structures

Cost and schedule management

Documentation management

Page 19: Building Low Cost Cubesat - GAUSS Srl · 2018. 2. 14. · Introduction - Why Cubesats? • The Cubesat model provides almost all of the benefits of a larger program at a fraction

Keep It Simple Stupid

Keep track of interfaces

Update risk analysis

Team work and respect of management plans and

ConOps

Conclusion & Futur Perspectives

4th IAA Conference on University Satellite Missions and Cubesat Workshop

Page 20: Building Low Cost Cubesat - GAUSS Srl · 2018. 2. 14. · Introduction - Why Cubesats? • The Cubesat model provides almost all of the benefits of a larger program at a fraction

Thank youfor your attention

4th IAA Conference on University Satellite

Missions and Cubesat WorkshopIAA-AAS-CU-17-06-02