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宇宙航空研究開発機構のスペースデブリ関連研究について

Overview of JAXA’s Space Debris related Research Activities

伊東康之 (宇宙航空研究開発機構)

Yasuyuki ITO, JAXA

Space debris is a risk factor for all the countries and organizations who perform space activities. For example, multiple collision damages are possible in a year for satellites with projected areas exceeding 10 m2. Efforts are required for mission assurance against debris. The protection design for critical components of a spacecraft, adding functions to complete self-disposal actions, etc.are considered. Almost all the debris experts in the world agree that the number of existing debris would continue to grow and the environment would go worse. Therfor, in addition to the mitigation efforts, more positive measures to remedy the environment should be globally discussed and implemented. In order to develop measures to remove debris, technology development is needed as well as international cooperation. Considering the above mentioned situation, JAXA’s debris related research activities are introduced in this presentation.

スペースデブリは宇宙開発利用活動を行うすべての国、機関にとってリスクとなっており、ミッシ ョンの成功を保証するために努力が必要である。一例として、高度

1000km

を周回する断面積

1m2

の衛星には

1mm

φのデブリが3年で1回の頻度で衝突すると推定されており、当たり所が悪いと人 工衛星の機能の一部を喪失することとなる。より大きいデブリが衝突すれば衛星自体の喪失、破砕 に至る。デブリは継続的に増加しており、その状況悪化の加速度を緩和するために、デブリ発生防 止対策を徹底しなければならない。多くの対策は既に世界的に合意されているが、用済み後のシス テムの除去や、落下時の地上安全の確保には更に徹底・配慮が必要な状況である。軌道上物体同士 の衝突は近年現実的な脅威となっており、現状のデブリ発生防止対策を超えて、分布密度の高い高 度域から使用済み衛星・ロケットを相当数除去する活動が、近い将来必要になるという認識が共有 されつつある。この様な状況を踏まえ、宇宙航空研究開発機構におけるデブリ関連研究を概観する。

Biography

ITO, Yasuyuki

Associate Director General, JAXA Place of birth : Osaka, Japan

Ms. and Bs. degree in Electrical Engineering at Kyoto University

1980 - 2003: National Space Development Agency (NASDA) 2003 - : JAXA

< R & D Career >

Earth Observation Instrumentation at R&D Directorate: Synthetic Aperture Radar, Microwave Radiometer Conceptual study of ENVISAT/AMI at ESA/ESTEC as Research Fellow

Earth Observation Satellite Project : ADEOS-II, Aqua/AMSR-E

< Administration/Management Career >

Strategic Planning Dept., Human Resources Dept., Audit & Evaluation Office, Earth Obs. Science Team Management

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December 2014

6 th Space Debris Workshop, Chofu, Tokyo Yasuyuki ITO, JAXA

OVERVIEW OF JAXA’S SPACE DEBRIS RELATED RESEARCH

ACTIVITIES

TABLE OF CONTENTS

1. about Space Debris

2. about Japan’s space policy and JAXA 3. Goals and Topics of JAXA Research

activities

Y.Ito : Dec.2014 2

6TH SPACE DEBRIS WS

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3

䝕䝤䝸ྜィᩘ

䝻䜿䝑䝖ୖẁᶵయ

⾨ᫍ

⇿Ⓨ◚∦㢮 ศ㞳ᨺฟ㒊ရ㢮

Increased by Chinese intentional destruction

Ref. NASA NewsJan. 2012 ᲢSize: LEO larger than 10 cm, GEO Larger than 1 mᲣ

+PETGCUGFD[EQNNNKUKQP QH75CPF4WUUKCP5%

Y.Ito : Dec.2014 6TH SPACE DEBRIS WS

Causes of Generation of Debris

4GH'5#4GRQTVVQ70%12715䠋565%(GD

5RCEGETCHV

Ტ1RGTCVKQPIQT FKURQUGFᲣ

4GNGCUGF 1DLGEVU

(TCIOGPVU

&KURQUGF.CWPEJ 8GJKENG

Y.Ito : Dec.2014 4

6TH SPACE DEBRIS WS

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Y.Ito : Dec. 2014 5

Estimated Annual Collision of Small Sized Debris to a Operating Satellite

( 1m 2 cross section at 800km altitude orbit )

Debris SIZE 0.1~1mm 1~10mm 1~10cm 10cm over Estimated Annual

Collision (times) 100 0.01* 0.0001 0.00001

Ref. 䠖Analysis using ESA tool “MASTER”

Measures for

Mission Assurance Protection Orbit Maneuver No measure

* NASA analysis shows 0.1

6TH SPACE DEBRIS WS

Basic Plan on Space Policy, Second Issue : January 2013 ( First Issue : June 2009 )

JAXA has been positioned as

the core organization that provides technical support for the entire governmental development and utilization of space projects.

Expanding the utilization of space

Basic Policy

Ensuring autonomy

National Security and Disaster Management

Priority Subjects Industrial

Development Progress in Frontier Areas including Space Science

6TH SPACE DEBRIS WS Y.Ito : Dec.2014 6

(5)

Table of Contents 0. Introduction

1. Current circumstances 2. Goals

3. Basic Policy

4. Measures that the Government should take

ؕஜ૾ᤆᴾ

6TH SPACE DEBRIS WS Y.Ito : Dec.2014 7

Basic Plan on Space Policy,

Draft for New Issue : for Public Comment in November 2014

Provisional Translation

4. Measures that the Government should take

(1) Systems of Governmental Measures for the Goal Ṟ Ensuring Security in Space

ϸὸ Sustainable Development and Utilization of Space

Space Situational Awareness (SSA) system acquisition and development of the capability

Capability for collision avoidance

Realize/strengthen the rule of law in space Development of technologies for debris removal

res that thee GGovernment should takke Gover Gov

Description about Space Debris in the New Basic Plan Draft

6TH SPACE DEBRIS WS Y.Ito : Dec. 2014 8

Provisional Translation

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9

Committee on National Space Policy

Y.Ito : Dec. 2014

Ref.: Presentation by Office of National Space Policy, CAO

6TH SPACE DEBRIS WS

JAXA ORGANIZATION CHART

Institute of

Aeronautical Technology Aerospace

Research &

Development Directorate

(ARD) Space

Transportation Mission Directorate

Satellite Applications

Mission Directorate I

Policy Coordination Admin. Management Technical Management Naoki

Okumura

Kiyoshi Higuchi

Human Spaceflight

Mission Directorate

Lunar &

Planetary Exploration

Program Group

President Senior Vice- President

IAF President

Institute of Space &

Astronauti Science cal

Y.Ito : Dec. 2014

6TH SPACE DEBRIS WS 10

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Y.Ito : Dec. 2014 11

JAXA Third Mid-T erm JAXA Second Mid- Te rm JAXA First Mid-T erm

2003

2013

1995 : NASA first Debris Standard 1999 ~ 2007 : CNES first Debris Standard

European Code of Conduct 2002 : IADC released the IADC Debris Mitigation Guidelines

2007 : UN adopted the COPUOS Debris Mitigation Guidelines

2011 : ISO released “Debris Mitigation Requirements”

2008

1996 : NASDA first Debris Standard

1999 : Japan proposed a specific committee to UNCOPUOS for debris issue

2006 : JAXA Debris Committee

2012 : ( Japan’s New Law )

< 6

th

Debris Workshop >

ISAS NAL NASDA

History of JAXA and World Debris Activities

6TH SPACE DEBRIS WS

Collision avoidance with manned system

㻌avoiding release of parts.

Limiting ejection of slag from solid motors

Avoiding release of 㻌

objects

Prohibition of intentional destruction, prevention

from break-ups Removal form protective

region at EOL

Protection from

impact of debris

Prevention of break-up

Avoiding collision

Ensuring re-entry safety Protection from

impact of tiny debris

Collision avoidance at

new launch

Collision avoidance with observable large

objects

Re-entry safety

Required measures for Debris Mitigation

Removal at EOL

Y.Ito : Dec. 2014 6th Space Debris WS 12

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Y.Ito : Dec. 2014 6th Space Debris WS 13

Major Elements of Strategy

Preventive Action

Detection

Counter Actions

Corrective Actions

䞉 Risk Identification э Observation, Modeling, Risk Analysis 䞉 Protection measures э Protection Design STD

䞉 Conjunction Assessment & Warning э Monitoring,

Conjunction Analysis 䞉 Impact & Failure detection э㻌 On-Board Detector

䞉 Preservation & Ground Safety э Mitigation Design &

Operation Re-entry Safety Analysis

䞉 Prevention of Chain Reaction э Technology for Removal Mission A ss ur ance Sustainable D ev el op m en t

Red : Primary R&D items,

Blue : Vehicles and spacecraft projects team will promote.

䞉 Collision Avoidance э Avoidance Maneuver

䞉 Damage Reduction э Separation of Function. etc.

14 14

Goals in next 5-year-plan

1. Objects smaller than 10 – 20 cm in GEO can be observed.

2. Conjunction with debris can be assessed by domestic facilities in sufficient precisions to support avoidance maneuver.

Mission Assurance: Ground Observation

Image of the automatic debris detection tool Y.Ito : Dec. 2014

6TH SPACE DEBRIS WS

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15 15

Mission Assurance: Modeling

Goals in Modeling

1. Future debris population can be prospected, and adequate policy can be implemented in advance.

2. Collision risk management will be conducted by analyzing the impact probability, damage estimation, and protection design. 㻌

Y.Ito : Dec. 2014

JAXA debris collision risk analysis tool, TURANDOT

6TH SPACE DEBRIS WS

16 16

Mission Assurance: Protection Design

Goals in next 5-year-plan

1. Establishment of a Protection Design Standard

• It enables adequate design depending on the mission characteristics.

Y.Ito : Dec. 2014 6TH SPACE DEBRIS WS

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17 17

Mission Assurance: Debris Detector

Goals in Debris Detector

1. The debris detector will be launched to confirm orbital debris distribution.

1. The debris larger than 100μm will be detected with its size

2. The data will contribute to the world debris models. 㻌

Disagreement in MASTER and ORDEM Y.Ito : Dec. 2014 6TH SPACE DEBRIS WS

18 18

Ground Safety

Goals in Ground Safety after deorbit

1. More reliable re-entry risk analysis can be done with improved database (material properties, human distribution, etc.) 2. Risky devices that

survive re-entry will be minimized.

Y.Ito : Dec. 2014 6TH SPACE DEBRIS WS

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19

Preservation and

improvement of the environment

Goals in Active Debris Removal 1. First step: Key technology

demonstration such as electro- dynamic tether (EDT) as

economical deorbit devices.

2. Final Step 䠖 large intact debris such as rocket upper stages will be removed by international

project.

6TH SPACE DEBRIS WS Y.Ito : Dec. 2014

Y.Ito : Dec. 2014 20

EDT Demonstration using HTV

EDT on HTV (H-II Transfer Vehicle)

„

Objective

„

Demonstration of EDT key technologies

„

Deployment of bare tether

„

Electron collection by bare tether

„

Electron emission by field emission cathode

„

Current loop formation via plasma

„

Autonomous current control operation

„

Flight Sequence

„

HTV leaves ISS and lowers altitude

„

Tether deployment

„

EDT operation

„

HTV re-enters atmosphere

End-mass

e

-

e

-

e

-

e

-

Tether

Electron emitter

HTV

Current

7 days

for EDT mission

6TH SPACE DEBRIS WS

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