Appendix 4 to esa ao/1-9225/18/NL/FF/gp

Family name	DOMÍNGUEZ	First name	DIEGO
Position	Researcher of Aerospace Research Group	Company	University of León
Phone number	[phone]	e-Mail	[e-mail]
Date of Birth	15/05/87	Nationality	Spanish
Relevant Experience
2014-today: Full-time lecturer at Department of Mechanics, Computing and Aerospace Engineering, University of León /Spain 2013-2014: Researcher at Vrije Universiteit Brussel, Engineering School, Brussels/Belgium 2008-2012: Researcher at Aerospace Engineering Area, Universidad de León Diego DOMÍNGUEZ joined the Aerospace Engineering Area of the University of León in 2008 after finishing his Bachelor’s Degree. Since then, he has taken part on multiple research projects. Within these projects, he has collaborated with multiple companies and research institutions from the aerospace sector, like the European Space Agency, Boeing Research & Technology Europe or Isdefe. Although his responsibilities have varied among the projects, they have been usually related with the numerical modelling and simulation. Then, he has developed several aerodynamic studies, as well as different design tasks for Unmanned Aerial Vehicles. He has been working not only in León, but in the Vrije Universiteit Brussel (VUB) for over a year, where he was in charge of teaching some aerospace courses as well as developing numerical simulations related with the wind energy sector. Once he came back to León in 2014, he occupied a full-time lecturer position. Diego has collaborated with Dr. Gonzalo developing services on micrometeorology (currently funded by Boeing R&T Europe), embedded flight management, planetary exploration based on aircrafts, propulsion of unmanned vehicles and disaster monitoring, mitigation and damage assessment. In 2016, Diego was one of the key personnel of the research group directed by Dr Gonzalo that was awarded with the ESA GSP HAPPIEST study to analyse the HAPS potential in communications and other complementary applications and to envisage a development roadmap. Author or co-author of 13 Scopus-indexed publications, 1 book and holding 1 patent on aerospace sciences.
Qualifications and Affiliations
Education and present position: PhD. Universidad de León, Aerospace Engineering Area Master of Research in Cybernetics, Universidad de León /Spain Bachelor’s Degree in Aerospace Engineering, Universidad de León /Spain Core Competences: Development and operation of autonomous airships Numerical modelling of continuum mechanics systems involving fluids and/or solids Lecturer on aerospace technologies (Rockets and Missiles, Propulsion Systems and Numerical Methods for Fluid Dynamics) Other competences: Wind energy Optimization Publications (selected): 2018 - “On the capabilities and limitations of high altitude pseudo-satellites”, J. Gonzalo, D. López, D. Domínguez, A. García, A. Escapa, Progress in Aerospace Sciences, Volume 70, p. 28-41. Elsevier 2017 - “High Altitude Pseudo-satellites: Proposal of Initiatives to Enhance Satellite Telecommunications (HAPPIEST): Final Report”, HAP-ULE-D1/02, ESA contract ESA contract No: 4000117605/16/NL/GLC 2015 - “Design of a hydroformed metal blade for vertical-axis wind turbines”, Domínguez Fernández, Diego and Pröhl, Marco and De Troyer, Tim and Werner, Markus and Runacres, Mark C. Journal of Renewable and Sustainable Energy (2015), Volume 7 2014 - “On the challenge of a century lifespan satellite”, Gonzalo, J., Domínguez, D., López D.. Progress in Aerospace Sciences (2014). Volume 70, Pages 28-41. (JCR 2014: 2.548) 2013 - “Lighter-Than-Air Particle Velocimetry for Wind Speed Profile Measurement”, J. Gonzalo; D. Domínguez; D. López, Renewable and Sustainable Energy Reviews. 33C, pp. 323 - 332. Elsevier SCI Ltd. ISSN 1364-0321
Languages: Spanish English Other associations expertise: Numerical Simulations Codes: OpenFOAM, Ansys, Matlab

Thales Alenia Space (TAS)

Catherine DESROCHES

Catherine Desroches is the design authority for the Stratobus product line from end 2017. She joined Thales Alenia Space in 1996 in the telecommunications domain, responsible for telecommunications payload and board/ground RF link for different S/C until 2005. From 2005 to 2009 she worked in the Galileo IOV system team. From 2009 to 2011, she worked at Thales underwater systems as system responsible for sonars. From 2011 to 2017 she held different system positions in the MTG team.

She holds a master’s degree in mathematics from Nantes University of Science and a n engineering degree from Ecole Supérieure Nationale des Télécommunications.

Marine Claeyman

Marine Claeyman is radiometric and spectral algorithm responsible of the Instrument Quality Tools of the Meteosat Third Generation. She is also algorithm expert for the Instrument Data Processing Facility (MTG operational ground segment). She joined Thales Alenia Space in 2011 to work in the MTG image quality team. From 2007 to 2010, she made a PhD at Meteo-France on the monitoring of air quality from space. She also participated to the redaction of the scientific justification report with a large scientific consortium for an Earth Explorer proposal for air quality monitoring from a geostationary orbit.

She holds a master’s degree in meteorology and remote sensing and an engineering from Seatech (former Institut des Sciences de l’Ingénieur de Toulon et du Var)

Family name	TONETTI	First name	STEFANIA
Position	Project Manager and Senior Mission Analyst	Company	Deimos Space S.L.U.
Phone number	[phone]	e-Mail	[e-mail]
Date of Birth	18 June 1982	Nationality	Italian
Relevant Experience
Stefania Tonetti graduated in Space Engineering and she has a PhD in Aerospace Engineering from Politecnico di Milano (Italy). In 2011 she joined Elecnor Deimos Space, where she is now Project Manager in the System Engineering and Earth Observation Mission Analysis Division of the Flight Systems Business Unit. Since 2011 she has worked on more than 20 Earth Observation mission studies, from phases 0 to C, mainly for ESA, the European Commission (FP7, H2020) or for the main European satellite manufacturing companies (Airbus Defence and Space, Thales Alenia Space, OHB). In 2015 she led the mission analysis activities of Deimos Space in the frame of the Phase B2 of the Copernicus Sentinel-5/UVNS, an instrument on-board MetOp-SG satellite to provide ozone profiles and columns, monitor various trace gases, monitor air quality and support climate monitoring.
Qualifications and Affiliations
Education and present position: 2015 - present Project Manager in the System Engineering & Earth Observation Mission Analysis Division of the Flight System Business Unit at Elecnor-Deimos 2011 - 2015 Project Engineer in the System Engineering & Earth Observation Mission Analysis Division of the Flight System Business Unit at Elecnor-Deimos 2008 - 2011 Ph.D. Aerospace Engineering, Politecnico di Milano, Italy 2004 - 2007 M.S. in Space Engineering, Politecnico di Milano, Italy 2001 - 2004 B.S. in Aerospace Engineering, Politecnico di Milano, Italy Core Competences: Mission Analysis for Earth Observation Missions. Competences: Project Management Programming Languages: Matlab, C++ Operating Systems: Windows Professional experience: Project Manager at DEIMOS and Mission Analysis Responsible for the “Copernicus Hyperspectral Imaging Mission for the Environment (CHIME) Phase A/B1 System Study” (Mar 2018 - present) Project Engineer at DEIMOS for the mission analysis activities of the “SKIM Earth Explorer Fast-Track Mission Phase A/B1 System Study” (May 2018 - present) Project Engineer at DEIMOS for the mission analysis activities in the “Phase A/B1 Study of the Copernicus High Spatio-Temporal Resolution Land Surface Temperature (LST) Monitoring Mission“ (Mar 2018 - present) Project Engineer at DEIMOS for the mission analysis activities in the H2020 project EO-ALERT “Next Generation Satellite Processing Chain for Rapid Civil Alerts” (Jan 2018 - present) Project Engineer at DEIMOS for the mission analysis activities of the UrtheDaily Constellation (2016 - present) Project Engineer at DEIMOS for the mission analysis activities of the OptiSAR Constellation (2016 - present) Project Engineer at DEIMOS for the mission analysis activities of the “SAT4EO System Engineering and Technology Prototype” (2016 - 2018) Project Manager at DEIMOS for the mission analysis and ground segment concept activities of the Next Generation Gravity Mission Phase 0 (2016 - 2017) Project Manager at DEIMOS and Mission Analysis Responsible for the H2020 project “Operational Network of Individual Observation Nodes” (2016 - 2017) Project Engineer for the in-orbit capability assessment and new mission identification in the “Disaster Risk Reduction using Innovative Data Exploitation Methods and Space Assets” (2015 – 2018) Project Manager at DEIMOS and Mission Analysis Responsible in the “Hybrid Propulsion Solutions for Space Debris Remediation Study” (2015 – 2016) Project Manager for DEIMOS activities and Mission Analysis Responsible in the "Copernicus Sentinel-5/UVNS Phase B2" (2015) Mission Analysis Responsible for the GNSS Reflectometry, Radio Occultation and Scatterometry on-board ISS (GEROS-ISS) - Phase A” (2014 – 2015) Project Engineer in the "Phase-A/B1 System Studies of the CarbonSat (2014 - 2015) and FLEX (2012 – 2015) Earth Explorer Opportunity Missions” Project Engineer for the “DEI2SIM Simulator: Fully Automated Mission Planning and Capacity Analysis Tool for the DEIMOS-2 Agile Satellite” (2014 – 2015) Mission Analysis Responsible in the "Assessment of Satellite Constellations for Monitoring the Variations in Earth Gravity Field " (2013 – 2015) Project Engineer in the “Design and Simulation Tool to demonstrate Data Products for Security Applications (DESIRE Study)” (2013 – 2015) Project Manager for DEIMOS activities and Mission Analysis Responsible for the "Terminal for Small S/C Application Phase C" (2014 - 2015) Project Engineer in the "Phase-B1 System Study of Biomass Earth Explorer Core Mission" (2013 - 2014) and in the “Biomass Phase-A Extension” (2012) Project Engineer in the "Ion Beam Shepherd IOD Mission Study" (2013 - 2014) Project Engineer for the development of the "Simulator for Moving Target Indicator Systems (SIMTISYS FP7)" (2011 - 2013) Project Engineer in the “DEIMOS-2 Mission Analysis and Simulation” (2011 – 2014) Project Engineer in the “GNSS-R Feasibility Study (Phase A)” (2011 - 2012) Project Engineer in the “Phase-A/B1 Study for GMES Sentinel-5” (2011 - 2012)

Family name	LOPEZ HONRUBIA	First name	FRANCISCO JESUS
Position	Project Manager	Company	Deimos Space S.L.U.
Phone number	[phone]	e-Mail	[e-mail]
Date of Birth	27 September 1970	Nationality	Spanish
Relevant Experience
Francisco Jesús Lopez graduated in Telecommunication Engineering at Universidad Politécnica de Valencia (Spain). After graduation he was a Young Graduate Trainee at ESA/ESTEC where he worked at the Ground Segment Division of the ENVISAT Project. In 1997 he joined Telefonica Sistemas to work on the Automation and Control Section on a Ground Station Automation System. In 1998 he joined GMV to work on the Mission Analysis Division to work on the ENVISAT Reference Operations Planning Facility. In 2001 co-founded Elecnor Deimos Space, where he is now Project Manager in the Ground Segment Business Unit. Since then he has worked in a large variety of projects mainly in the Mission Planning domain and more recently in the integration of Ground Segment systems for Earth Observation missions. He is currently working in the ground segment activities of several Phase A/B1 system studies for future ESA Earth Observation missions.
Qualifications and Affiliations
Education and present position: 2015 - present Project Manager in the Ground Segment Business Unit at Elecnor-Deimos 2005 - 2015 Technical and AIT Manager in the Ground Segment Business Unit at Elecnor-Deimos 2001 - 2005 Project Engineer in the Ground Segment Business Unit at Elecnor-Deimos 1998 - 2001 Project Engineer in the Mission Analysis Division at GMV 1997 - 1998 Project Engineer in the Automation and Control section of Telefónica Sistemas 1995 - 1997 Young Graduate Trainee at ESA/ESTEC 1988 - 1994 M.S. in Telecommunications Engineering, Universidad Politecnica de Valencia, Spain Core Competences: Mission Planning for Earth Observation Missions. Competences: Project Management Programming Languages: C++ Operating Systems: Windows, Linux Professional experience: Project Engineer at DEIMOS for the ground segment activities of the Phase A/B1 System studies of “SKIM Earth Explorer Fast-Track Mission”, “Copernicus Hyperspectral Imaging Mission for the Environment (CHIME)”, “Far-infrared-Outgoing-Radiation Understanding and Monitoring (FORUM)” and “Land Surface Temperature Monitoring (LTSM)” (May 2018 - present) AIT Manager at DEIMOS for a Direct Receiving Station for DEIMOS-2 (Jun 2016 – Apr 2018) Project Manager at DEIMOS for the AEOLUS Mission Management and Planning Facility (Jun 2015 – Dec 2017) On-site support at ESA/ESRIN with the Sentinel-2 PDGS Engineering Team (Jun 2013 – Jun 2015) AIT Manager at DEIMOS for the PDGS of DEIMOS-2 (Jan 2013 – Apr 2015) Technical Manager at DEIMOS for the Ground Station Control System for DEIMOS-2 (Apr 2011 – Jun 2013) Study Manager at DEIMOS for the Post-EPS Ground Segment Phase A Study on Mission Planning, Flight Dynamics and Calibration and Validation (Jan 2011 – Oct 2012) Technical Manager at DEIMOS for the GMES Service Coordinated Interface (Oct 2008 – Dec 2010) Technical Manager at DEIMOS for the GMES Product Harmonisation Phase 1 (Nov 2007 – Oct 2008) Technical Manager at DEIMOS for the Galileo Raw Data Generator (RDG) (Apr 2005 – Nov 2007) Project Engineer at DEIMOS for the Refence Planning Facility (RPF) of Cryosat (Jun 2003 – Mar 2005) Project Engineer at DEIMOS for the Galileo Ground Segment Preliminary Data Model (Jun 2002 – Jun 2003) On-site support at ESTEC for the operation of the RGT of ENVISAT (Mar 2002 – May 2002) Project Engineer at DEIMOS for the maintenance of the RGT of ENVISAT (June 2001 – Mar 2002) Project Engineer at GMV for the Reference Operations Planning Generation Tool (RGT) of ENVISAT (May 1998 – May 2001) Project Engineer at Telefónica Sistemas for the Monitoring and Control System of the Kiruna Satellite Tracking Ground Station (Sep 1997 – Apr 1998)

3. 
   Rationale of the proposed industrial organisation
   

[Optional: in case of Sub-contractor(s), the reasons for your choice]
Thales Alenia Space (TAS)
Thales Alenia Space France (TAS) is recognized as one of the World leaders in space systems design and development, covering the complete range of system activities, from global system architecture to operations concepts, mastering both space and ground segments. Over the past 40 years, being Prime for more than 80 spacecraft’s and contributing to more than 200 Satellites has allow reaching a position of European leadership. Partner of leading industry and satellite operators, TAS-F is contributing to most of the important programmes now in progress in a wide range of domains: Telecommunications, Navigation, Earth Observation, Science and Interplanetary Missions. To guarantee a successful development of these projects, TAS has a created a Business Line (see below).

In particular, TAS-F has an extensive heritage of successful Satellite Missions and instruments development for both institutional and commercial customers, and features an exceptional blend of experiences covering:

• 
  long-standing experience in ESA observation missions, for both Prime Contractor ships and Instruments, demonstrating a clear capacity to master all features of observation Satellites and Instruments.
  
• 
  operational, long-duration mission series flown on 3 generations of Meteosats, proving a demonstrated know-how in handling long-term storage, obsolescence and perennial knowledge over missions in orbit over dozens of years.
  
• 
  constellation series integration demonstrated know-how (world unique experience on Globalstar-2, O3B, Iridium) validating specific AIV detailed processes capable to guarantee on-time.
  
• 
  Small PROTEUS-based satellites development for CNES and NASA missions (CALIPSO, Jason, CoRoT, SMOS).
  
• 
  An extensive experience in design studies, particularly in Earth Observation missions of all classes to the European Space Agency
  

The satellites developed for ESA’s Herschel/Planck, MTG or Sentinel-1 and 3 projects not only demonstrate TAS-F capability to manage large and challenging programs, but also large industrial consortia, as well its capability to handle cryogenics, multiple payloads or high-level pointing with competence and success.

Ten years ago, Thales Alenia Space decided to develop a HAPS LTA platform, the Stratobus^TM, to complete and leverage its satellite offers, both for Telecommunication, Observation and Navigation missions. Studies were led from 2010 on feasibility, missions characterization and customer’s needs, internally founded and then supported by the French government (Plan d’Investissement d’Avenir) from 2016. Thales Alenia Space is currently the leader of a consortia in charge to develop the first full scale Stratobus^TM and then perform in flight validation tests in 2021.
Through its development, TAS acquired a world expertize on the HAPS, as well from the point of view of the necessary technologies, as the logistical means to be used, as missions and market knowledge. These knowledge will be put at the disposal of the consortium to make a quality study.

TAS-F HAPS Stratobus system as communication centre.

This envisaged contract is an opportunity for Thales Alenia Space to better understand the need of high-resolution, long-term measurements of air quality and GHG on urban scale, and evaluate they can potentially be realized with existing concepts and technologies using High Altitude Pseudo Satellites (HAPS).
Moreover, based on the results of the interaction with users, to evaluate a priliminary air quality or GHG Stratobus^TM mission concept, which includes identifying objectives, data products and synergies with existing and future satellite observation by assessing available or planned technologies. A demonstration flight can be proposed with Stratobus^TM PFM equipped with Air Quality or GHG instruments, on a use case, for example over a major European city, metropolitan or industrial area.

Key success factors	TAS Relevant Background	Illustration
Prime Contractor and Platform provider to several small and medium sized Earth Observation Missions	Prime of Sentinel-3 Prime of Sentinel-1 Prime of Cosmo-Skymed (TAS-I) Jason 1, 2, 3 COROT SMOS	Sentinel 3
Long Life Time highly reliable satellite Stream lined series production Latest Generation Avionics	Globalsat-2 (qualified for 15 years in LEO, launched on 19/10/2010) IRIDIUM NEXT (2nd generation)	Prime of 2nd generation constellations
Relevant instrument experience for IR instruments design & accommodation	Prime of OLCI on Sentinel-3 Prime of IASI (on METOP) Prime of SMOS Satellite, JASON …. Prime of MTG FCI Prime of HR instruments	IASI SMOS
Deep Understanding of Ground Segment and Operations	Prime of Earth Observation Satellite and related ground segment (MSG) Prime of defence telecommunication systems (SYRACUSE) Defence observation system (Cosmo-Skymed) (TAS-I) Prime of METOP Ground segment Prime of Sentinel 2 PDGS	EPS Ground Segment
Prime of European Space Programs and complete familiarity of European Standards and Geo-return considerations	Meteosat, MSG and MTG Herschel & Planck	Herschel MSG

TAS-F relevant experience in ESA missions.

2. 
   PLANNING
   

1. 
   Proposed schedule and milestones
   

The project runs for 12 months. HAPS milestones are given in the table below, while the time schedule is provided as bar chart in section 2.2.2

Milestone ID	Milestone Title	Relative timeline
KO	Kick-off	T0
MTR	Mid Term Review	T0+6
FM	Final Meeting	T0+12

2. 
   Bar chart
   

The overall project planning is given in the bar chart below. Minutes of meetings are not included in the table. The WP and Task titles are found in the WBS at 1.3.2.1 above.

	T0	T0+2	T0+4	T0+6	T0+8	T0+10	T0+12
WP/ TASK id	KO	PM1	PM2	MTR	PM3	PM4	FM
WP1000			URD+TN1
WP2000					UCD
WP3000							MRD
WP4000							PRM
WP5000							ERS+FRP+CCD
Meeting
Web-meeting

All deliverables are planned at end of each WP, and will be reviewed during the progress meetings. The requested documentation and deliverables will be made available to the ESA Technical Officer (TO) two weeks ahead of each meeting, in order to allow enough time for review. The deliverables are fully compliant with the SoW and the Draft Contract.

3. 
   LIST OF DELIVERABLE ITEMS – SPECIFICATION OF ANY NON-CONFORMANCE
   

1. 
   Deliverable Items
   

DOC id	Title	Due Date	Deliver to	Remarks
URD
TN1
UCD
MRD
PRM
ERS
FRP
CCD

……………

2. 
   Non-conformances / limitations / additions regarding deliverable items
   

None

3. 
   FINANCIAL PART
   

1. 
   PRICE QUOTATION FOR THE CONTEMPLATED CONTRACT:
   

The total price offered for the proposed work as a response to the

ESA AO/1-9225/18/NL/FF/gp is 250 000 EURO.

2. 
   SUB-CONTRACTING PLAN
   

The tendering team and the resulting price breakdown is as follows:

Table X: Sub-contracting plan, including WPs lead by partner

Company	ESA Entity Code	P/Prime S/Subcontractor	Country	Total (EUR)	WPs
NILU - Norwegian Institute for Air Research	1000005237	P	NO	89 900	WP1000, WP4000,WP5000
UNILEON – University of Leon	1000024262	S	ES	50 000	WP2000
DEIMOS	1000006221	S	ES	60 000	WP3000
Thales Alenia Space France	1000003108	S	FR	50 100

3. 
   DETAILED PRICE BREAKDOWN
   

1. 
   PSS costing forms:
   

For PSS costing forms see annexes.

2. 
   Milestone Payment Plan
   

The HAPS milestone payment plan is closely linked to the project milestones. The milestone payment plan is provided in Table X

Table X: Milestone payment plan

Milestone (MS) Description	Schedule Date	Payments from ESA to (Prime) Contractor (in Euro)	Country (ISO code)
KO: Start of Activity	T0	87 500 EUR (35% of total)	NO
MS 1: Mid Term Review. Upon successful completion of WP1000 and successful review and acceptance of URD + TN1, and	To +6 months	112 500 EUR (45% of total)
Final Settlement MS 2: Upon the Agency’s acceptance of all deliverable items due under the Contract and the Contractor’s fulfilment of all other contractual obligations including submission of the Contract Closure Documentation	To + 12 months	50 000 EUR (20% of total)
TOTAL		250 000 EUR

It is suggested that a payment will take place at KO and start of activity, upon signature of the contract by both parties.

Table X: Milestone payment plan for the Sub contractors.

For information purposes only:

For Information purposes only : Amounts in Euro for Contractor and Sub-contractor(s)
Milestone	Prime Contractor NILU	Insert Country (ISO code) NO	Sub-contractor A ULEON	Insert Country (ISO code) ES	Sub-contractor B DEIMOS	Insert Country (ISO code) ES	Sub-contractor C TAS-F	Insert Country (ISO code) FR
KO	31 465		17 500		21 000		17 535
MS-1	40 455		22 500		27 000		22 545
MS-2	17 980		10 000		12 000		10 020
TOTAL	89 900		50 000		60 000		50 100

3. 
   Travel and subsistence plan
   

The project travel plan is presented in Table X. Meetings are connected to milestones and deliverables which will be reviewed at meetings. The schedule is consistent with the SoW and the project planning (Figure X). Company rules for travel expenses will apply to travel and subsistence expenses. The travel plan for each project partner is provided in Exhibit B to PSS A2.

Table X: Meeting schedule including both physical meetings and web meetings.

Meeting	Timing	Location	Attendance
KO	T0	Web meeting	NILU, ULEON, DEIMOS, TAS-F
PM1	T0+2	Web meeting	NILU, ULEON, DEIMOS, TAS-F
PM2	T0+4	Europe	NILU, ULEON, DEIMOS, TAS-F
MTR	T0+6	Web meeting	NILU, ULEON, DEIMOS, TAS-F
PM3	T0+8	Web meeting	NILU, ULEON, DEIMOS, TAS-F
PM4	T0+10	Web meeting	NILU, ULEON, DEIMOS, TAS-F
FM	T0+12	ESA ESRIN	NILU, ULEON, DEIMOS, TAS-F

4. 
   CONTRACT CONDITIONS PART :
   

1. 
   BACKGROUND INTELLECTUAL PROPERTY RIGHTS
   

Table X: Project partners Intellectual Property Rights

Exact name of BIPR Item	Owner	Description	Patent # or Ref. / Issue / Revision / Version #	Contract / Funding Details under which the IPR was created	Date of creation of the version of the BIPR listed here	Licence	Affected deliverable with comments	Protected Format (Y/N)
Stratobus^TM	TAS-F	Stratobus Platform dirigible architecture concept.		Internal funding			D2 Technical Note HAPS Stratobus^TM design included D3 UCD Stratobus^TM operation included	Y

2. 
   SPECIFICATION OF ALL INPUTS TO ENTER INTO THE BLANKS EXISTING IN THE DRAFT CONTRACT
   

Inputs to enter into the blanks in the draft contract are provided in Table X

Table X: Inputs to draft contract

Article/Page/Clause	Blank	Input
Front page	Contractor	NILU – Norwegian Institute for Air Research
Page 1	Contractor	NILU – Norwegian Institute for Air Research
Page 1	Registered office	P.O.Box 100 N-2027 Kjeller, Norway
Page 1	Represented by its	Director of Finance
Page 1	Ms/Mr	Ms. Eva Beate Andresen
Article 1.3.2		To be done upon contract negotiation
Article 1.3.3	City, Country	Lillestrøm, Norway
Article 3.1	Total price	250 000 Euro
Article 3.1	Table	See Table X
Article 5.1.2	Contractor address	NILU – Norwegian Institute for Air Research P.O.Box 100 N-2027 Kjeller, Norway
Article 5.1.2 a)	Contact person for technical matters	Ann Mari Fjaeraa Telephone [phone] e-mail [e-mail]
Article 5.1.2 b)	Contact person for contractual and administrative matters	Eva Beate Andresen Telephone [phone] e-mail [e-mail] with copy to Ann Mari Fjaeraa Telephone [phone] e-mail [e-mail]

3. 
   OTHER REMARKS ON THE DRAFT CONTRACT
   

No other remarks.

4. 
   MANAGEMENT AND ADMINISTRATIVE COMPLIANCE MATRIX
   

The HAPS proposal complies fully with all ESA management and administrative requirements including those listed in Table X

Table X: Management and administrative compliance matrix

REQUIREMENT (*)	COMPLIANT (Y/N/P) (**)	REMARKS (***)
M01 3.1 Management	Y
M02 3.2 Reporting	Y
M03 3.3 Meetings	Y
M03 3.5 Deliverables	Y

(*) Reference is made to SoW

(**) Compliance (Y), non-compliance (N) or partial compliance (P) with respect to each requirement;

(***) Any relevant remarks and, for partial compliance cases (P), an explanation/justification
___________________________________

ATTACHMENTS:

ANNEX 1: Signed PSS-A2 form. Please see separate attachment

Signed PSS-A8 form. Please see separate attachment

ANNEX 2: DESCRIPTION OF TENDERER’S FACILITIES FOR THE EXECUTION OF THE WORK