Ariane 5 User Manual Issue 5

Posted on 12/10/2017by admin

Ariane 5 User’s Manual. The Ariane 5 is tailored to the increasingly diversified demand for service including heavier and larger satellites, a wider range of orbits. User’s Manual. Issue 5 Revision 1 July 2011 Ariane 5 User’s Manual Issue 5 Revision 1 July 2011 Issued and approved by Arianespace Edouard PEREZ Senior Vice. Ariane 5 User Manual Issue 5 PDF Download Summary: Filesize 60,98MB Ariane 5 User Manual Issue 5 PDF Download Hunting for Ariane 5 User Manual Issue 5 Do you really.

Ariane 5 User’s Manual Ariane 5 User’s Manual Issue 5 Revision 1 Table of contents Preface Foreword Configuration control sheet Table of contents Acronyms, abbreviations and definitions CHAPTER 1. INTRODUCTION 1.1. Purpose of the User’s Manual 1.2.

European Space Transportation System 1.3. Arianespace launch services 1.4. Ariane launch vehicle family - History 1.5. Launch system description 1.5.1. Launch vehicle general data 1.5.2. European spaceport and CSG facilities 1.5.3. Launch service organisation 1.6.

Corporate organization 1.6.1. Arianespace 1.6.2.

Partners 1.6.3. European space transportation system organization 1.6.4. Main suppliers 1.6.4.1. Astrium ST 1.6.4.2. Snecma (SAFRAN Group) 1.6.4.3. RUAG Space 1.6.4.4.

Europropulsion CHAPTER 2. PERFORMANCE AND LAUNCH MISSION 2.1. Introduction 2.2. Performance definition 2.3. Typical mission profile 2.4. General performance data 2.4.1.

Geosynchronous transfer orbit missions 2.4.2. SSO and polar circular orbits 2.4.3. Elliptical orbit missions 2.4.4.

Earth escape missions 2.4.5. International Space Station orbit 2.5.

Injections accuracy 2.6. Mission duration 2.7.

Launch windows 2.7.1. Definitions 2.7.2. Process for launch window definition 2.7.3. Launch window for GTO dual launches 2.7.4.

Launch window for GTO single launches 2.7.5. Launch window for non GTO launches 2.7.6. Launch postponement 2.7.7.

Engine shutdown before lift-off 2.8. Spacecraft orientation during the ascent phase 2.9. Separation conditions 2.9.1.

Orientation performance 2.9.2. Separation mode and pointing accuracy 2.9.2.1. Three axis stabilized mode 2.9.2.2. Spin stabilized mode 2.9.3. Separation linear velocities and collision risk avoidance 2.9.4. Multi-separation capabilities Arianespace© 0.5 Ariane 5 User’s Manual Issue 5 Revision 1 CHAPTER 3.

ENVIRONMENTAL CONDITIONS 3.1. Mechanical environment 3.2.1.

Static acceleration 3.2.1.1. On ground 3.2.1.2. In flight 3.2.2. Steady state angular motion 3.2.3. Sine-equivalent dynamics 3.2.4. Random vibration 3.2.5. Acoustic vibration 3.2.5.1.

On ground 3. Msa Toxgard Ii Manual. 2.5.2. In flight 3.2.6.

Shocks 3.2.7. Static pressure under the fairing 3.2.7.1. On ground 3.2.7.2. In flight 3.3. Thermal environment 3.3.1. Introduction 3.3.2. Ground operations 3.3.2.1.

CSG facility environments 3.3.2.2. Thermal condition under the fairing or the SYLDA 5 3.3.3. Flight environment 3.3.3.1. Thermal conditions before fairing jettisoning 3.3.3.2. Aerothermal flux and thermal conditions after fairing jettisoning 3.3.3.3. Other fluxes 3.4.

Cleanliness and contamination 3.4.1. Cleanliness level in environment 3.4.2.

Deposited contamination 3.4.2.1. Particule contamination 3.4.2.2. Organic contamination 3.5. Electromagnetic environment 3.5.1. L/V and range RF systems 3.5.2.

The electromagnetic field 3.6. Environment verification CHAPTER 4.

SPACECRAFT DESIGN AND VERIFICATION REQUIREMENTS 4.1. Introduction 4.2. Design requirements 4.2.1. Safety requirements 4.2.2. Selection of spacecraft materials 4.2.3. Spacecraft properties 4.2.3.1. Payload mass and CoG limits 4.2.3.2.

Static unbalance 4.2.3.3. Dynamic unbalance 4.2.3.4. Frequency requirements 4.2.4.

Dimensioning loads 4.2.4.1. The design load factors 4.2.4.2.

Line loads peaking 4.2.4.3. Handling loads during ground operations 4.2.4.4. Dynamic loads 4.2.5. Spacecraft RF emission 4.3. Spacecraft compatibility verification requirements 4.3.1.

Verification logic 4.3.2. Safety factors 4.3.3. Spacecraft compatibility tests 4.3.3.1. Static tests 4.3.3.2.