opto -pyrotechnical technology for space …

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This document is the property of EADS SPACE Transportation and shall not be communicated to third parties and/or reproduced without prior written agreement. Its contents shall not be disclosed. © - EADS SPACE Transportation - 2005 Problem Statement for Launch Vehicles October 5 & 6th, 2005 OPTO OPTO - - PYROTECHNICAL TECHNOLOGY PYROTECHNICAL TECHNOLOGY FOR SPACE APPLICATIONS FOR SPACE APPLICATIONS

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This document is the property of EADS SPACE Transportation and shall not be communicated to third parties and/or reproduced without prior written agreement.

Its contents shall not be disclosed. © - EADS SPACE Transportation - 2005

Problem Statement for Launch Vehicles

October 5 & 6th, 2005

OPTOOPTO--PYROTECHNICAL TECHNOLOGYPYROTECHNICAL TECHNOLOGY

FOR SPACE APPLICATIONSFOR SPACE APPLICATIONS

Page 2 TE6 0511 This document is the property of EADS SPACE Transportation and shall not be communicated to third parties and/or reproduced without prior written agreement.

Its contents shall not be disclosed. © - EADS SPACE Transportation - 2005

Pyrotechnical Subsystem on Ariane 5 (1/3)Current status

� The current A5 ECA configuration includes:

� 369 pyrotechnical devices (including 515 meters of pyro-

transmission line) – this number would noticeably decrease

thanks to opto-pyro technology

� 79 final functions to be activated which shall remain unchanged

� The safeguard rules require two independant subsystems:

� One dedicated to neutralisation

� One for functional and operational needs

U Compliance with current safeguard requirements is still to be

achieved through dedicated studies, which could direct the

architecture selection

Page 3 TE6 0511 This document is the property of EADS SPACE Transportation and shall not be communicated to third parties and/or reproduced without prior written agreement.

Its contents shall not be disclosed. © - EADS SPACE Transportation - 2005

515 meters of pyro transmission cords

over 189 lines

17 Arming & Safety Devices

36 IFOC

30 RMV

34 detonators

Pyrotechnical Subsystem on Ariane 5 (2/3) Current status (cont’d)

BSA: Boîtier de Sécurité et d’Armement (Safe & Arm Box)RMV: Relais MultiVoies (MultiPath Relays)IFOC: Inflammateur à Fonctionnement par Onde de Choc (Detonation to Deflagration Initiator)

Page 4 TE6 0511 This document is the property of EADS SPACE Transportation and shall not be communicated to third parties and/or reproduced without prior written agreement.

Its contents shall not be disclosed. © - EADS SPACE Transportation - 2005

� Main objectives associated with Optopyrotechnics

�Recurring Cost reduction (at both system and pyro-subsystem levels)

�Only a technological breakthrough can bring about new cost savings (removal of pyrocords, multipath relays,…)

�RAMS :

• Removal of primary explosives from the system

- should lead to decrease the dangerousness at system level (after demonstration of security requirements)

- should simplify the last operations (additional cost saving)

• Immunity to Electro-Magnetic Interference (EMI) and Electrical Static Discharge (ESD)

- increase the safety

�Mass reduction

Pyrotechnical Subsystem on Ariane 5 (3/3)Objectives / Advantages

Page 5 TE6 0511 This document is the property of EADS SPACE Transportation and shall not be communicated to third parties and/or reproduced without prior written agreement.

Its contents shall not be disclosed. © - EADS SPACE Transportation - 2005

Optopyrotechnical Subsystem (1/3)Principle

� The optopyrotechnics project consists in replacing the current electro-pyrotechnical chains by electro-opto-pyrotechnical chains

Detonator –DOPInitiator - IOP

FT

SwitchOptical Interception

Barrier

DLDL

Laser diode

Optical

Fiber

BSAAD

LT LTRMV

Electro-pyrotechnical elementary chain

(Electro-)opto-pyrotechnical elementary chain

Relais Multi-Voies

Pyrotechnical Transmission Line

FT

Final function(Fonction Terminale)

ElectricalDetonator

OpticalDetonator/Initiator

Electrical Interception

Barrieror

Page 6 TE6 0511 This document is the property of EADS SPACE Transportation and shall not be communicated to third parties and/or reproduced without prior written agreement.

Its contents shall not be disclosed. © - EADS SPACE Transportation - 2005

� The major concern of the opto-pyro technology is Optical Power Transmission through FiberOptic

�which is somewhat different from the well-known Optical Data

Transmission

• Optical Data Transmission has been mastered for years in

aeronautics:

- Basic rules such as routing, …remain valid for Power application

- Space environment may be more severe (in particular launch

vehicles)

• Optical Power Transmission raises new problems still to be

solved

� More over, compliance of components, specially optical ones, with harsh environment is not assessed

Optopyrotechnical Subsystem (2/3)Major concerns

Page 7 TE6 0511 This document is the property of EADS SPACE Transportation and shall not be communicated to third parties and/or reproduced without prior written agreement.

Its contents shall not be disclosed. © - EADS SPACE Transportation - 2005

�Moving from electro-pyrotechnics to opto-pyrotechnics has several impacts:

• « visible » at Stages level:

- Layout

- Pyrotechnics sub-system simplification,…

• less « visible », at System level:

- Transient phases studies for control of Stages separation (and ignition): simultaneity of commands

- Fulfilling Safeguard requirements

- Impacts on On-Board Flight S/W which manages Ordnance commands

� Switching toward optopyrotechnic is not only a

technological step, but also impacts system aspects:

• overall design, manufacturing, testability and AIT (Assembly Integration Test) process from the early beginning

Optopyrotechnical Subsystem (3/3)Problem Statement