Announcement of Opportunity for Hosted Payload on board EDRS-C - - PowerPoint PPT Presentation

ESA UNCLASSIFIED – For Official Use

Announcement of Opportunity for Hosted Payload on board EDRS-C SATELLITE

ESA-ESTEC 22/09/2011

ESA UNCLASSIFIED – For Official Use

HOSTED PAYLOAD ON BOARD EDRS-C SATELLITE

• AGENDA

09:00 Arrival and registration 09:15 Welcome address 09:30 EDRS programme 10:00 Announcement of Opportunity process

10:45 Coffee break

11:00 EDRS-C satellite Hosted Payload embarkation 11:30 Q&A open session

12:30 Lunch

14:00 30 minute Q&A individual sessions 17:30 End of workshop

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3

Basic EO trends:

• Higher resolution

and new wavelength ! higher data volumes

• Congestion in traditional

telecom means (X-band)

• Need for near-real-time

data and rapid tasking EDRS capabilities:

• Increased contact time
• Higher data rates
• Higher capacity
• Flexible data distribution

EDRS programme basic principles

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4

Service-oriented approach:

• Operational system able to fulfil user requirements with required

service availability (redundancy)

• Open system able to serve all interested user communities with

different technologies to meet different needs

Public-Private Partnership:

• Selection of EDRS Operator / Service Provider
• Operator owner of EDRS system infrastructure
• Commitment to operate EDRS system
• Provide services to ESA users
• Commercialise data relay services to all interested user

communities

Foster creation of data relay market

EDRS programme basic principles

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5

Data relay services retrieving data from LEO satellites to ground – Very high data rate at 1.8 Giga bit per second through optical Inter- satellite Link (ISL) – High data rate of 600 Mega bit per second (Mbps) through optical ISL (possibility of data encryption on board GEO) – Medium data rate 150-300 Mbps through Ka ISL – Data provided to customers either directly to EDRS ground station (5-6 m antenna) installed on User Premises or via terrestrial links from EDRS Central Hubs Rapid Tasking service re-programming LEO satellites – A few kilo bits per second through optical ISL – Up to 1 Mbps through Ka ISL

EDRS targeted services

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6

ESA as “anchor user”: GMES programme provides start-up user

• Data relay service for Sentinel-1+2 for min. 50% of mission data
• Embarkation of data relay terminal
• EDRS system deployment in time with Sentinel constellation launch

schedule

• Operational showcase for other potential users

Any other potential EO operator and in particular military EO systems

EDRS targeted Users

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7 USER platform equipped with a EDRS User Space Terminal (UST) EDRS Mission & Operation Centre (MOC) EDRS GEO Payloads EDRS Feeder link Ground Station (FLGS)

TM/TC

EDRS Satellite Control Centre (SCC) USER Mission and Operation Center USER Ground Station (UGS)

Management data User data

EDRS User Space Segment

EDRS system architecture

TM/TC

Data relay Rapid tasking

USER data processing premises

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EDRS Space Segment architecture

8

Space segment formed by 2 elements: Piggyback payload (EDRS-A)

• On board commercial operator satellite to guarantee early in-orbit system

element (by 2014) available to provide services to first users (GMES) Dedicated satellite (EDRS-C)

• Fully controlled by EDRS Operator (by 2015)

=> High service availability through in orbit redundancy Possible extension if required by user demand (not covered by currently defined programme)

• Other payloads to address other users’ needs (e.g. S-band)
• Additional elements (higher system capacity and/or availability)

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EDRS system Capabilities

9

Through EDRS-A piggy back payload:

– Optical ISL data relay services (1.8 Gbps/600 Mbps) – Optical ISL rapid tasking services (few kbps, through Eutelsat GEO encrypted TM/TC link) – Ka ISL data relay services (up to 300 Mbps) – Ka ISL rapid tasking service (up to 1 Mbps through dedicated RF data link) – High performance Feeder Link in Ka EESS bands (26 GHz) with European coverage – By-passable data encryption for the optical data relay service at 600 Mbps only

Through EDRS-C satellite:

– Optical data relay services (1.8 Gbps/600 Mbps) – Optical rapid tasking services (few kbps, through ASV EDRS-C GEO encrypted TM/TC link) – No Ka ISL relay services – High performance Feeder Link in Ka EESS bands (26 GHz) with European coverage – By-passable data encryption for the optical data relay service at 600 Mbps only

ESA UNCLASSIFIED – For Official Use

HOSTED PAYLOAD ON BOARD EDRS-C SATELLITE

09:00 Arrival and registration 09:15 Welcome address 09:30 EDRS programme 10:00 Announcement of Opportunity process

10:45 Coffee break

11:00 EDRS-C satellite Hosted Payload embarkation 11:30 Q&A open session

12:30 Lunch

14:00 30 minute Q&A individual sessions 17:30 End of workshop

ESA UNCLASSIFIED – For Official Use

AO process - Objectives and Principles

" Available resource on EDRS-C (power, mass, volume) is an opportunity to fly additional payloads " Does not need to be innovative or telecom related payload " “Embarkation” fee charged to the Hosted Payload provider covering:

• Integration of the HP onto the host satellite,
• Support of the host satellite manufacturer for ground testing,
• Launch & LEOP,
• Support of the host satellite manufacturer for IOT (command and control tasks)

" Will bring needed financial contribution to the tight EDRS budget " Conditions for the provision of the hosted payload will be agreed in a “Mission Implementation Agreement” between ESA and the HP provider " Operations fee to be agreed with EDRS operator in a separate agreement

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AO process - Funding

" Embarkation fee

• The payload proponent must come with available funds to pay for

the embarkation fee

• Any source of funding private/public can be considered
• Total/partial ESA contribution possible but needs to be backed up

with relevant ESA programme/directorate and corresponding national delegation " The development cost of the payload is outside the AO hosting Mission Implementation Agreement

• Could be partially covered by other parallel ESA development

contract to be indicated in the proposals

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AO process - Mission Implementation Agreement main principles

" Hosted Payload will be a Customer Furnished Item (CFI) to be provided by the Proponent to the Agency, which will provide it to the EDRS Operator for integration and embarkation " Ownership of the HP will remain with the HP Provider " Intellectual Property Rights vested in the HP Provider will remain with the HP provider " Exclusive access and exploitation rights of the HP by the HP provider will be subject to separate Operational agreement between the HP Provider and the EDRS Operator " In case the HP is delivered late, the HP provider undertakes to deliver a dummy payload at no cost " Related frequency filing/licensing will be the responsibility of the HP Provider. " DRAFT MIA will be provided to down-selected proponents as a basis for the dialogue phase before final proposal submission

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AO process - Schedule

AO issued on 11th August 2011 1. 15th Sept - Notice of Intent to be submitted 2. 22nd Sept - Workshop for information dissemination and Q&A sessions (including one to one sessions) 3. 21st October - Submission of proposal 4. Initial down selection 5. Technical and contractual dialogue 6. 15th December - Final proposal submission 7. Final selection and negotiation in December/January

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AO process - Key Inputs / Outputs

HP Providers

!

"#! $%&'! ()*)+,-!

!

Workshop

Update of reqt

• IRD-1
• Draft MIA

Proposal submission Final Proposal submission

• ICD-0
• HPTP-0
• MIA

"#!./'0*! ()*)+1%'!

HP contract signature inputs to EDRS-C PDR EDRS-C PDR ICD-1 HPTP-1

2011

Sept Aug Oct Nov Jan Dec Mar Feb Apr May June

2012

AO issued including

• IRD-0

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AO process - Key Inputs/Outputs

" The proposal for the 21st of October no longer requires a statement of compliance to the IRD-0. The rest of the proposal guidelines (chapter 8) remains valid.

• The IRD-0 provided in the AO is indicative and not yet final
• The C-band mission was removed from the EDRS-C satellite since issuing the AO

" Additional inputs will be provided following first down-selection of HP proponents:

• An updated IRD-1
• and a draft MIA

" Following a Technical and Contractual dialogue, the final proposal will need to include additional key documents

• HP ICD version 0
• Hosted payload Test Plan (AIT and IOT ) version 0
• Revised Mission Implementation Agreement

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AO process - Key message for selection

" First down selection will be mainly based on

• Initial assessment of compatibility with EDRS-C (technical +

programmatic)

• Risk assessment (technical + programmatic)
• Evidence of funding coverage (public and/or private) of all

mission elements (payload, embarkation, operations) on the basis of letters of support from funding sources (private/ public)

• Level of compliance with contractual principles

# Evidence of funding is often missing, it is key to provide a convincing proposal on this particular aspect

ESA UNCLASSIFIED – For Official Use

AO process - Key message for selection

" Same main criteria will apply with a more detailed and more mature proposal in particular with regards to

• the MIA including the rights and obligations between ESA and

the HP providers

• Final and solid evidence of funding

ESA UNCLASSIFIED – For Official Use

HOSTED PAYLOAD ON BOARD EDRS-C SATELLITE

09:00 Arrival and registration 09:15 Welcome address 09:30 EDRS programme 10:00 Announcement of Opportunity process

10:45 Coffee break

11:00 EDRS-C satellite Hosted Payload embarkation 11:30 Q&A open session

12:30 Lunch

14:00 30 minute Q&A individual sessions 17:30 End of workshop

Akos Hegyi / Hosted Payload Workshop 22.9.2011

EDRS-C Input for Hosted Payload Candidates

Date - 2

EDRS-C Orbital position: Drivers

• European coverage of the feeder downlink
• Visibility of EO satellites that are over the desired observation areas

Priority 1 & 2: Africa & Asia Lower priority: South America, Europe, Other world regions

• Feasibility of frequency coordination

For EDRS feeder downlink (EESS frequency) For TT&C frequency (on-going trade off between Ka and Ka bands

Current preferred orbital position (TBC): 22.5 E (alternatively 22 – 24 E) Orbital position can be reviewed for Hosted Payloads as long as

• Above drivers are respected
• Orbital position can be quickly frozen

Date - 3

• Proposed feeder downlink service coverage

Ground Service area (for EDRS-Mission + TT&C)

Date - 4

Proposed EDRS Coverage Diagram

• Coverage for EDRS-A @ 9°E & EDRS-C @ 22.5°E

EDRS-C - Hosted Payload Workshop

22.09.2011, ESA – ESTEC, Noordwijk

Content

! Hosted Payload Budgets (Mass and Power) ! GERD ! Accommodation: Dimensions, Payload Module, Reflector ! Electrical Interfaces: TM/TC budget, PMU ! AIT & Schedule ! Conclusion

EDRS-C Hosted Payload Budgets

! EDRS-C Satellite and Payload configuration has majorly changed

• removal of electrical propulsion
• removal of Telecom payload

The resulting dedicated Satellite EDRS-C available total payload resources are:

• Mass 290 kg and DC Power 2500 W (EOL)

The Data Relay (DR) Payload including Laser Communication Terminal requires:

• Mass 130 kg and DC Power 800 W (EOL) – estimated mass

The remaining satellite resources available to the Hosted Payload:

• Mass 160 kg and DC Power 1700 W (EOL)

OHB System AG / Titel der Präsentation / Datum Seite 3

GERD – General Equipment Requirements Document

The SGEO Platform General Equipment Requirements Document (GERD) specifies:

• General Design & Interfaces
• Mechanical Design & Interfaces
• Thermal Design & Interfaces
• Electrical Design & Interfaces
• Environmental Requirements (On Ground, Launch and In Orbit)
• Verification by Testing (Sequence, Conditions, Loads, etc.) & Analysis

The GERD will be provided after:

• Signed NDA between Tender and OHB

Seite 4 OHB System AG / EDRS-C Hosted Payload Workshop

Accommodation

OHB System AG / Titel der Präsentation / Datum Seite 5

Satellite Overview

OHB System AG / Titel der Präsentation / Datum Seite 6

Satellite Dimensions

OHB System AG / Titel der Präsentation / Datum Seite 7

Payload Module Accommodation Earth Deck: used by LCT and Ka Feeder, available for Feeder North Panel: used for Data Relay Payload and LCT Radiator South Panel: available for Hosted Payload

Seite 8 OHB System AG / EDRS-C Hosted Payload Workshop

Typical Heat Zone distribution Up to 18 (9+9) Conduction Cooled TWTAs Up to 12 (6+6) Radiation Cooled TWTAs

Antenna Accommodation

• Available to Hosted Payload:
• ne side deployable reflector
• Reflector maximum size

2.5 m for a rigid reflector 2.15 m dual gridded shell

• Feeder to be installed on earth deck
• Receivers and LNAs Equipments on

Cold Zone (Extension)

Seite 9 OHB System AG / EDRS-C Hosted Payload Workshop

Electrical Interfaces

OHB System AG / Titel der Präsentation / Datum Seite 10

Architecture

OHB System AG / Titel der Präsentation / Datum Seite 11

PCDU

Electrical Interfaces to the Platform

OHB System AG / Titel der Präsentation / Datum Seite 12

SGEO (PCDU)

Available PMU Interfaces / Budget (updated)

Seite 13 OHB System AG / EDRS-C Hosted Payload Workshop

HV-HPC HC-HPC ! 351

TM budget TC budget

TSM RSM ASM BDM BSM ! 36 ! 12 ! 32 MIL-STD-1553B ! 7 50V Power Supply Heaters ! 51 ! 45

Serial interfaces Power Distribution Lines

AIT & Schedule

OHB System AG / Titel der Präsentation / Datum Seite 14

EDRS-C Master Schedule

The EDRS program will be realized with the following schedule 11/2011 Satellite SRR 30.04.2012 Satellite PDR Datapack Delivery to Customer 07/2012 Satellite PDR closure 10/2013 Satellite CDR 01/2014 Start of Payload AIT (Data Relay and Hosted Payload) 07/2014 Start of Satellite AIT Q1&2/2015

• Env. Test Campaign

End of 2015 Launch

OHB System AG / Titel der Präsentation / Datum Seite 15

Conclusion

OHB System AG / Titel der Präsentation / Datum Seite 16

Conclusion / Summary

! EDRS-C Satellite and Payload configuration has majorly changed

• removal of electrical propulsion
• removal of Telecom payload

!The EDRS-C Satellite provides 290 kg & 2.5 kW of resources

• Estimated Resources available to Hosted Payload 160 kg & 1.7 kW

! Accommodation can be realized with

• Complete South Panel (up to 18 CC-TWTAs)
• Side deployable reflector up to 2.5 m single shell (new)

! Electrical Interfaces are between Hosted Payload and Platform to PMU and PCDU

• Details to be clarified in IRD-1

! EDRS-C Master Schedule

• ICDs of Hosted Payload needed for PDR and CDR on Satellite level
• Start of Payload AIT required at 01/2014
• Launch end of 2015 (latest)

Seite 17 OHB System AG / EDRS-C Hosted Payload Workshop