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The Insurance Institute of London The Insurance Institute of London CII CPD accredited - demonstrates the quality of an event and that it meets CII/PFS member CPD scheme requirements. This webinar will count as 1 hour of CPD and can be included as part of your CPD requirement should you consider it relevant to your professional development needs. It is recommended that you keep any evidence of the CPD activity you have completed and upload copies to the recording tool as the CII may ask to see this if your record is selected for review. MHI Launch Services - key essence of MHI’s quality management - Ref. B01038001405 February 17, 2021 © MITSUBISHI HEAVY INDUSTRIES, LTD. All Rights Reserved. MHI PROPRIETARY INFORMATION MHI PROPRIETARY INFORMATION 1. Introduction of MHI & Insurance Activities for our products 2. Launch Services 2.1 current work force H-IIA/B 2.2 Next gen, flagship H3 - Under Development - 3. MHI Quality Management Overview 4. Overcoming anomalies ４.1 Launch Operation case, H-IIB F8 ４.2 Development case, H3 main engine(LE-9) 5. Conclusion © MITSUBISHI HEAVY INDUSTRIES, LTD. All Rights Reserved. PROPRIETARY INFORMATION 3 1. Introduction of MHI & Insurance Activities for our products MHI PROPRIETARY Introduction of MHI INFORMATION Power Systems Foundation July 7, 1884 Capital (USD) 2,415 MUSD As of Mar. 2019 Employees Thermal Power Plant Compressor CO2 Recovery Plants Desalination Plant (consolidated) 80,744 As of Mar. 2019 Industry & Infrastructure Sales (consolidated) 38,055 MUSD As of Mar. 2020 EBITDA 115.1 Dubai Metro Intelligent Transport Systems Overseas offices 7 Aircraft, Defense & Space Currency rate: USD 1 = JPY 110 Boeing – 787 Space Jet Defense Aircraft Launch Vehicle (Composite main wings) (H-IIA/-IIB) © MITSUBISHI HEAVY INDUSTRIES, LTD. All Rights Reserved. PROPRIETARY INFORMATION 4 1. Introduction of MHI & Insurance Activities for our products MHI Major Products and Services of Space Systems PROPRIETARY INFORMATION Launch Vehicle Space Station / HTV (c)JAXA Space Station HTV HTV-X On-orbit Experimental Unit Satellite Satellite Launch Services Rocket Engine Space Vehicle Launch Vehicle Development (c)JAXA Next Gen. Small Satellite (c)JAXA Ground Facility Attitude Control System Reusable Launch Vehicle © MITSUBISHI HEAVY INDUSTRIES, LTD. All Rights Reserved. PROPRIETARY INFORMATION 5 1. Introduction of MHI & Insurance Activities for our products MHI PROPRIETARY Insurance activities for MHI’s product INFORMATION Global Insurance program Similar risks across group companies are covered efficiently under Global Insurance program. 106 105 104 103 102 101 100 10-1 Mass production Build to Order Space Jet Nuclear power Generation Turbocharger Fighter Launch Services Thermal Fork lift plant Air conditioner insufficient contract Product term recall Damage cased by accident Insufficient Anomaly of Gas turbine construction the product capability © MITSUBISHI HEAVY INDUSTRIES, LTD. All Rights Reserved. PROPRIETARY INFORMATION 6 1. Introduction of MHI & Insurance Activities for our products MHI PROPRIETARY Types of Insurance for Launch Services INFORMATION Each Risk in all procedure of Launch Services is covered by Insurance respectively. Contract Launch Launch + 1 year Launch Services Marine Launch In-orbit Property Insurance Pre-launch Insurance Insurance Insurance Insurance CGL(Commercial General Liability) Insurance TPL for 2nd TPL(Third Party Liability) Insurance stage Insurance by LSP Insurance by Operator Manufacturing Shipping Launch Campaign General Insurance Specialty Insurance Manufacturing/shipping risks are covered Launch campaign risk is underwritten by under Global Insurance Program. TMNF/ JAIP (Japanese Aviation Insurance Pool), then ceded to the international space insurance market including Lloyd’s. © MITSUBISHI HEAVY INDUSTRIES, LTD. All Rights Reserved. PROPRIETARY INFORMATION 7 2. Launch Services MHI PROPRIETARY 2. Launch Services INFORMATION LV family for MHI Launch Services H3 Key Concept Competitive Pricing Flexibility for Commercial Customers Reliability established by technology heritage since H-IIA Total length: Approx. 63m Core vehicle diameter : 5.2m Booster diameter : 2.5m Performance: 7 tons (to GTO) Maiden flight in 2021 H-IIA H-IIB H3 Commercial services starting in 2022 H2A202 H2A204 H3-30 H3-22 H3-24 © MITSUBISHI HEAVY INDUSTRIES, LTD. All Rights Reserved. PROPRIETARY INFORMATION 8 2. Launch Services MHI PROPRIETARY 2.1 current work force H-II A/B INFORMATION Services We Provide Coordination of satellite- launch vehicle interface MHI Launch Services Customer Contract JAXA (Japan Aerospace Exploration Agency) • Program Management • Range Safety / Control • Mission Integration Operation • Down Range Operations • Vehicle Manufacturing • Launch Facility Maintenance • Mission Modification • Technical Support • Launch Campaign Authorization of various controls Insurance against potential launch failure Manufacture of subsystems & components (export, use of explosives, etc.) Other Manufacturers Space Insurance Government Community Offices Brokers, underwriters © MITSUBISHI HEAVY INDUSTRIES, LTD. All Rights Reserved. PROPRIETARY INFORMATION 9 2. Launch Services MHI PROPRIETARY 2.1 current work force H-II A/B INFORMATION Transportation of the Satellite Customer Satellites Arrive at International Airport in Japan Tobishima Plant Chubu- Centrair International Airport Customer/ Satellite Manufacturer Approx. 2-3 days Transportation to Tanegashima Launch Site Spacecraft Facility at Launch Site © MITSUBISHI HEAVY INDUSTRIES, LTD. All Rights Reserved. PROPRIETARY INFORMATION 10 2. Launch Services MHI PROPRIETARY 2.1 current work force H-II A/B INFORMATION Tanegashima Space Center Vehicle Assemble Building (VAB) Launch Pad Launch Pad No.2 (LP2) No.1 (LP1) Modification to H3 <For H-IIB> <For H-IIA> pad in progress View from Observation Deck Observation Deck (3km from Launch Pad) H-IIA © MITSUBISHI HEAVY INDUSTRIES, LTD. All Rights Reserved. PROPRIETARY INFORMATION 11 2. Launch Services MHI PROPRIETARY 2.1 current work force H-II A/B INFORMATION Number of anomalies No. of launch vehicle anomalies during launch campaign H-IIA MHI Launch Services after F13 60 50 Example: 40 Sensor malfunction → replace with an alternative sensor Small scratch → smoothen and apply surface coating 30 20 10 0 Flight No. H-IIB MHI Launch Services after F4 The number of anomalies are kept very 30 25 low by stringent quality control for both 20 H-IIA and H-IIB Launch Services. 15 10 5 0 BTF1 BF2 BF3 BF4 BF5 BF6 BF7 BF8 BF9 Flight No. On-Time Launch Anomaly：Nonconformance to the spec requirement (include specific trend data) © MITSUBISHI HEAVY INDUSTRIES, LTD. All Rights Reserved. PROPRIETARY INFORMATION 12 MHI PROPRIETARY INFORMATION Video (1) MHI Launch Services © MITSUBISHI HEAVY INDUSTRIES, LTD. All Rights Reserved. PROPRIETARY INFORMATION 13 2. Launch Services MHI PROPRIETARY 2.2 Next gen, flagship H3 - Under Development - INFORMATION Technology Heritage from H-IIA & H-IIB New development based on Minor update of H-IIA H-IIB current technology current technology (heritage succession) (e.g. cost reduction) H-IIA/B Fairing Larger fairing 5.2 m diameter 2nd stage engine (LE-5B-2) 2nd stage engine [Expander (LE-5B-3) Bleed Cycle] Core diameter Same (5.2m) Core diameter SRB SRB (SRB-A) (SRB-3) st 1st stage engine 1 stage engine (LE-7A) (LE-9) [Staged Combustion [Expander Bleed Cycle] Cycle] 1st stage engine 1st stage engine clustering (2units) clustering (2 or 3 units) © MITSUBISHI HEAVY INDUSTRIES, LTD. All Rights Reserved. PROPRIETARY INFORMATION 14 2. Launch Services MHI PROPRIETARY 2.2 Next gen, flagship H3 - Under Development - INFORMATION H3 development status 1st Stage BFT (Battleship Firing Test) 1st stage propulsion system function were verified, in 2018-2019 ・Engine steady-state properties (100% and throttle) ・Engine start-up/cut-off and transient properties ・Tank pressure control function ・Engine gimbal control function ・Dynamic properties of propulsion system stage ・Vibration and thermal environment for components st 1 Test Stand © MITSUBISHI HEAVY INDUSTRIES, LTD. All Rights Reserved. PROPRIETARY INFORMATION 15 2. Launch Services MHI PROPRIETARY 2.2 Next gen, flagship H3 - Under Development - INFORMATION H3 development status 2nd Stage CFT (Captive Firing Test) 2nd stage system function were verified in 2020. ・3 firings test with flight hardware flawlessly conducted. ・Cumulative 1500sec. (Flight Full Duration 660s) ・ 1st, 2nd Ignition simulation nd 2 stage @JAXA © MITSUBISHI HEAVY INDUSTRIES, LTD. All Rights Reserved. PROPRIETARY INFORMATION 16 2. Launch Services MHI PROPRIETARY 2.2 Next gen, flagship H3 - Under Development - INFORMATION H3 development status_Maiden Flight 2021 TF1 Launch Vehicle Manufacturing • The launch vehicle for Test Flight was assembled in Tobishima Plant, Nagoya. • All function tests, including avionics functions /signal transmission from sensors / propulsion functions (pipes and valves) , have been successfully completed. • Launch vehicle was transported to the Tanegashima Launch Site. @JAXA @JAXA TF1 Launch Vehicle assembled in 2 LE-9 engines for H3-22 configuration Tobishima Plant, Nagoya © MITSUBISHI HEAVY INDUSTRIES, LTD. All Rights Reserved. PROPRIETARY INFORMATION 17 MHI PROPRIETARY INFORMATION Video (2) H3 Development © MITSUBISHI HEAVY INDUSTRIES, LTD. All Rights Reserved. PROPRIETARY INFORMATION 18 3. MHI Quality Management Overview MHI PROPRIETARY MHI Quality Management Overview INFORMATION (1) Based on International/Japanese/JAXA’s standard and MHI’s quality policy (2) Additional quality improvement
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