To Long Life Satellite Application of JAXA EEE Parts ...(6) JERG-2-023 ( Long Life Satellite Application of JAXA EEE Parts Handbook forSpace Transferable Parts ) was issued on May

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Total Service Provider Ryoei Technica Corporation MITSUBISHI ELECTRIC Group

Total Service ProviderRyoei Technica Corporation

To Long Life Satellite Application of JAXA EEE Parts Handbook for Space Transferable Parts

Affiliation: Ryoei Technica Co.

26th microelectronics workshop October 24, 2013; Tsukuba International Congress Center Space Application Study for Space Transferable

Parts (Chapter of Long-Life Satellite)

Chairperson: Sumio Matsuda

This presentation uses the result of "the space application committee of Space Transferable Parts " where it is hosted by JAXA held in 2011FY and 2012FY.

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Total Service Provider Ryoei Technica Corporation MITSUBISHI ELECTRIC Group CONTENTS

1. Definition of “Space Transferable Parts “

2. Background

3. Current Status

4. Space Radiation Environment

5. Application of Space Transferable Parts to Satellite

6. Attention of Space Transferable Parts in Space

7. Considered Subjects to apply Space Transferable Parts to Space

8. Space application Basic Flow of Space Transferable Parts

9. Summary

JERG-2-023 ( Long Life Satellite Application of JAXA EEE Parts Handbook for Space Transferable Parts ) was issued on May 21,2013. This handbook is referred RNC-CNES-Q-ST-60-100(General Requirements for the use of Commercial EEE Parts in Space Applications) of CNES and PEM-INST-001(Instructions for Plastic Encapsulated Microcircuit (PEM) Selection, Screening, and Qualification) of GSFC/NASA.

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All parts Parts for space

COTS High reliablity parts Industrial parts Parts for car

Standard part (JAXA Qualified parts) Non-standard part (NSPAR parts) and JAXA development strategy parts

for submarine cable for nuclear power, and for aircraft etc.

For toy/for game etc. (Impact damage small when breaking down)

For factory equipment/infrastructure (Impact damage large when breaking down)

For engine control etc. (Parts affected to life)

All parts Parts for space

Space Transferable Parts High reliablity parts Industrial parts Parts for car COTS

Standard part (JAXA recognition parts) Non-standard part (NSPAR parts) and JAXA development strategy parts

for submarine cable for nuclear power, and for aircraft etc

For toy/for game etc. (Impact damage small when breaking down)

For factory equipment/infrastructure (Impact damage large when breaking down)

For engine control etc. (Parts affected to life)

COTS

OLD

NEW

1. Definition of “Space Transferable Parts”

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Total Service Provider Ryoei Technica Corporation MITSUBISHI ELECTRIC Group 2. Background

(1) Rapid Advance of Semiconductor Technology.

(2) Small size, High Accumulation, High Speed, High Performance, and Energy-Saving Technology.

(3) Strong Needs of Satellite for Small Size, High Performance, and Energy-Saving.

(4) Satellite with Self-Subsistence, Flexibility at Small Size, Light Weight for Promotion.

(5) Industrialization of Space related company is promoted consequently.

(6) Requirement of Speedy Satellites Development.

(7) The good use of Space Transferrable Ground Parts for Suitable Small Size, Light Weight, Price Reduction, Shortening of Development Period.

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Total Service Provider Ryoei Technica Corporation MITSUBISHI ELECTRIC Group 3. Current Status

(1) End of east and west cold war. (1989) (2) Launch of MDS-1(Mission Demonstration test Satellite-1) by JAXA (Mainly COTS evaluation satellite). (2002) (3) Rise up opportunity of positively uses COTS (Qualification Method changes QPL→OML in DOD/USA) . (4) Issue Space Application Standard of COTS by French Space Agency (CNES). (5) JERG-0-052 (Common Application of JAXA EEE Parts Handbook for Space Transferable Parts ) was issued on May 11,2012. (6) JERG-2-023 ( Long Life Satellite Application of JAXA EEE Parts Handbook forSpace Transferable Parts) was issued on May 21,2013. (7) Scientific Satellite Application of JAXA EEE Parts Handbook for Space Transferable Parts is investigated in Fiscal year 2013.

MDS-1: This figure is JAXA provided

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vibration and shock, at launch

･High energy (Electron) (Proton)

･Atomic oxygen

･Space radiation (Solar proton)

･High energy (Electron)

･Ultraviolet rays

･Radiation belt

(Inner belt)

･Vacuum ･Microgravity

〔Magnetosphere〕･Radiation belt

(Outer belt)

･Space debris

〔The atmosphere〕

･Cosmic rays

・Vacuum ・Micro gravity

・Extreme temperature cycling (90 minutes /cycle,

6000 cycle/ year)

・Vacuum ・Micro gravity

・Extreme temperature cycling ・Electrification, Electrical discharge

【GEO】

This figure is JAXA provided.

4. Space Radiation Environment

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Satellite

Mission Equipment

Space Transferable Parts

ーーーー※1

BUS Equipment

Space Qualified Parts(JAXA,ESA.MIL)

(Power Supply, Attitude control system etc.)

(Observation system etc.)

※1: Space Transferable Parts also to the bus equipment in a specific project are used.

・Satellite important parts：Parts of influence success or failure or security needs (safe the ground and payload safety) for mission directly in bus equipments and mission equipments of long-life satellite. (Quality assurance level Class I Equivalent)

・Other parts for satellite：Parts of influence other elements at experimental equipments other trouble of equipments (measurement system for reference data acquisition) that don’t influence success or failure of mission directly even if it is bus equipments or mission equipments of long-life satellite. (Quality assurance level Class II Equivalent and over)

・Parts for experimental equipment：Parts of proving space with new development equipments or improved equipments. (Class III Equivalent and over ）

Space Qualified Parts(JAXA,ESA.MIL)

5. Application of Space Transferable Parts to Satellite

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(1) Though the use of the space transferable parts technology is indispensable, attention is necessary for the use of space transferable parts.

(a) Narrow Temperature Range (b) Lack of Radiation Tolerance and High Vacuum performance (c) Frequently Design Change and Evaluation Necessary. (d) Parts User have to evaluate Space Transferable Parts. (2) Evaluation of the lot to apply is indispensable and additional cost needed.

6. Attention of Space Transferable Parts in space

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(1) Necessity of timely evaluation about Parts Performance, because life Cycles of Parts are short. (especially, Reliability and Radiation Tolerance) (2) Necessity of JAXA EEE Parts Handbook for Space Transferable Parts (criteria) for timely evaluation. (3) Necessity of Comparison between Ground Test Data and Space Flight Data. (Mainly Radiation Tolerance Data for Publication of above handbook) (4) Necessity to carry out the revision of the handbook for Progress of Parts Technology and for Comparison between ground evaluation test and space flight experience continuously. (5) Necessity of Mutual Agreement (Cooperation) of Parts User (System/ Eequipment Manufacturers) and Parts Manufacturers.

7. Considered subjects to apply to Space Transferable Parts to Space

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Necessity/Requirement of satellite (function and

mission requirement, etc.)

Are there standard parts or

non-standard parts?

Are there candidate parts that to Space Transferable Parts?

Confirmation of cooperation intention with part manufacturer

(a)Project requirement (b) design requirement (c) manufacturing requirement (d) operation requirement

Selection criteria (a)Space Transferable Parts shall be select in the condition of

technical and economical difficulty for selection from standard parts and non-standard parts(NSPAR).

(b) In the case of the choice of candidate parts, parts user manufacturers confirm information about the validity of the latest data of the parts manufacturers, qualification applicability, defect notice, warning information and suitability of parts application.

(a)Necessity of prior approval, the document (memo etc.) is needed when using parts for the particular application such as satellite . (b)Parts user (system/equipment manufacturers) needs the detailed data for the selection of design, mounting, and quality/reliability performance etc.

①

②

③

④

8. Space Application Basic Flow of Space Transferable Parts

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Does it not conflict with prohibition and restrictions in the prescribed space application in HDBK?

(a) Failure rate (b) Temperature range (c) Prohibition and restriction matter in selection and application (d) Radiation tolerance (e) Derating

Dose-Depth Curve: This figure is JAXA provided.

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8. Space Application Basic Flow of Space Transferable Parts (continue)

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Request to Parts Manufacturer about application and design information disclosure

Memo (idea) adjustment/mutual agreement with part manufacturer

Acquisition of information disclosure/data requirement

Issue of procurement specification (data sheet use)

NSPAR application

Procurement adjustment ⇔ contract memo/order

(a) Candidate parts and approval parts lists (i) The candidate parts used by the project are selected, and user (system/equipment manufacturers ) issues and maintains the part list (approval parts list). (ii) The candidate parts also identified to "Space application non-standard part" added to the parts list (approval parts list) at the critical design review (CDR) . Furthermore, these candidate parts are checked by JAXA for NSPAR as "space application non-standard parts”. NSPAR: Non-Standard Parts Approval Request (b) Evaluation of candidate parts Parts user (system / equipment manufacturers ) plans an evaluation about candidate parts and carries it out, when evidences(information from the parts manufacturers for the initial evaluation) do not receive from the parts manufacturers .

⑥

⑦

⑧

⑨

⑩

⑪


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Screening/LAT

Receiving inspection/ data evaluation

Reflection and assembly/examination to instrument design

Keep/re-inspection of surplus goods

Disposition alert

For defect/failure analysis (Correspond with the reliability program)

(a) Procurement Specification

In the case of parts procurement, the procurement specification is provided for the candidate parts and they are procured based on this specification.

(b)Screening Test (c) Lot Acceptance Test (LAT) (d) Radiation Test (e) Receiving Inspection (f) Destruction Physical Analysis (DPA) (g) Handling and Storage (h) Re-inspection (i)Traceability (j) Defect and Failure (k) Alert

⑫

⑬

⑭

⑮

⑯

⑰

(b),(c),(d) and (g) are referred RNC-CNES-Q-ST-60-100(General Requirements for the use of Commercial EEE Parts in Space Applications) of CNES and Instructions for EEE Parts Selection, Screening, Qualification ,and Derating) of GSFC/NASA.

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Total Service Provider Ryoei Technica Corporation MITSUBISHI ELECTRIC Group 9. Summary

1.The space application committee of Space Transferable Parts issued JERG-2- 023 ( Long Life Satellite Application of JAXA EEE Parts Handbook for Space Transferable Parts ) was issued on May 21,2013. But it is necessary to note that it is not a guideline.

2. This handbook was issued that supplement collects standard parts for space and flight proven parts (NSPAR parts), and it is expected that new subjects and improve points become clear by really applying this handbook. 3. In the deliberation of the Handbook Study Committee, Collaborative Relationship (Relationship of Mutual Trust) between User (System /Equipment) Manufacturers and Parts Manufacturers are build, the Circle of Space Committee has extended.

4. JAXA has been studied Scientific Satellite Application of JAXA EEE Parts Handbook for Space Transferable Parts in 2013FY.

5. In addition, Investigation Committee of JAXA-PPL Preparation Activity starts in 2013FY.

Acknowledgements: The author would like to thank member of “the space application committee of Transferable Parts " for their helpful insights and assistance.

Documents

To Long Life Satellite Application of JAXA EEE Parts ...(6) JERG-2-023 ( Long Life Satellite Application of JAXA EEE Parts Handbook forSpace Transferable Parts ) was issued on May