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Project Management:
Brazilian Experience

   Himilcon de Castro Carvalho, AEB




                                      Used with Permission
“Classic”
Project Phasing
  & Planning
           1 yr   2-3 yrs   ECSS or ISO
Reality
Activity or $$




                      1-2 yr   2-3 yr         4-6 yr

                                                        Lack of:

                                                        Budget
                                                        Human Resources

                                                        Infrastructure




                 decision mobilization peak            launch &
                                                       ops
Reality
Activity or $$




                      1-2 yr      2-3 yr         4-6 yr

                                                                    Lack of:

                                                                    Budget
                                                                    Human Resources

                                                                    Infrastructure




                 decision mobilization peak                         launch &
                                              Gov't Changes         ops
                      Political   OK!         Economical crisis
                      talks       Let's go    Changes in priorities
Reality
                                                   What was
                                                   expected
Activity or $$




                      1-2 yr      2-3 yr         4-6 yr

                                                                    Lack of:

                                                                    Budget
                                                                    Human Resources

                                                                    Infrastructure




                 decision mobilization peak                         launch &
                                              Govn't Changes        ops
                      Political   OK!         Economical crisis
                      talks       Let's go!   Changes in priorities
Project Organization
                 Strong Matrix Structure
                 (80' – 90')
                               Mech.   Electr.. Ground AIT QA   ...
                               Eng.    Eng.     Segment



Project Office




       Project Office = Management + Systems Engineering

       QA, AIT, Ground Seg. completely dedicated to this single
       project
Project Organization

                   Weak Matrix Structure
                   (90' – 00')
                     Systems     Mech.   Electr.. Ground AIT   QA   ...
                     Eng.        Eng.    Eng.     Segment



Project Office 1
Project Office 2
Project Office 3



  Competition for project resources, human resources and budget
Planning

     Scope         Scope                                                Schedule
                                  WBS
    Planning      Definition                                             Devel.



  Risk Mgt.         Cost           HR          Activity     Activity
    Plan          Estimating    Planning      Definition   Resources

    Risk            Cost
Identification    Budgeting                    Activity      Activity
                                              Sequencing     Duration
   Qualit.          Quality
  Risk An.         Planning

  Quant.           Comm.
  Risk An.         Planning

Risk Resp.        Plan Purch.     Plan
 Planning           & Acq.      Contracting
“out of control” variables

                 Planning                                  “under relative control”
                                                           variables



     Scope         Scope                                                       Schedule
                                  WBS
    Planning      Definition                                                    Devel.



  Risk Mgt.         Cost           HR          Activity          Activity
    Plan          Estimating    Planning      Definition        Resources

    Risk            Cost
Identification    Budgeting                    Activity            Activity
                                              Sequencing           Duration
   Qualit.          Quality
  Risk An.         Planning

  Quant.           Comm.
  Risk An.         Planning

Risk Resp.        Plan Purch.     Plan
 Planning           & Acq.      Contracting
“out of control” variables

                 Planning                                  “under relative control”
                                                           variables
                                                           and        focus


     Scope         Scope                                                       Schedule
                                  WBS
    Planning      Definition                                                    Devel.



  Risk Mgt.         Cost           HR          Activity           Activity
    Plan          Estimating    Planning      Definition         Resources

    Risk            Cost
Identification    Budgeting                    Activity            Activity
                                              Sequencing           Duration
   Qualit.          Quality
  Risk An.         Planning

  Quant.           Comm.
  Risk An.         Planning

Risk Resp.        Plan Purch.     Plan
 Planning           & Acq.      Contracting
Impacts

PM under severe HR and Budget Restrictions

 Low responsivity
 Schedules not used as actual management tool

 Small number of concurrent projects

 Low industry dynamics




 Focus on WBS
 Focus on Activity Definition & Sequencing

 Focus on Quality/Verification Planning

 Special focus on Risk Planning
Thank you!


 Himilcon de Castro Carvalho
 Director of Space Policy and Strategic Investments
 Brazilian Space Agency
 himilcon@aeb.gov.br
Mini-SAR
An Imaging Radar on India’s Chandrayaan-1 Mission to the Moon




                                       Paul D. Spudis
                                   MSR Principal Investigator

                                  Lunar and Planetary Institute
                                          Houston TX

                                        spudis@lpi.usra.edu

                                  www.spudislunarresources.com

               NASA Program Management Challenge 2010
                            February 2010
                                                                  1
Origins

Waikaloa, Hawaii 2003
  Dr. Narendra Bhandari talk on proposed Chandrayaan-1
     mission (not yet selected for flight)
  I approach him to fly radar; he encourages it
  APL submits unsolicited letter proposal
  ISRO decides on open competition for foreign payloads
     (< 10 kg, < 100 W), Feb. 2004
  Submit formal proposal, April 2004
  Selected for flight, September 2004




                                                      2
Approval
Getting the money from NASA
   Technology interest from SOMD; exploration interest from ESMD
   Technology development package developed and jointly funded
Getting approval from Dept. of State
   Present instrument concept/overview to DoS Dec. 2004
   Formal application for export license Jan. 2005
   State approval June 2005
Getting final approval from ISRO
   TAA draft sent to ISRO in June 2005; no response
   Continuous delay; demand for change of title of TAA document
   TAA signed during May 2006 India visit by M. Griffin (NASA
     Administrator)



                                                                   3
Build and test

Mini-SAR (re-named Mini-RF) gets
  underway May 2005; instrument
  PDR Dec. 2005
Chandrayaan/MSR ICD draft
  written and approved Nov. 2005
Mini-SAR CDR Sept. 2006
Chandrayaan-1 CDR May 2007
Mini-SAR ship to APL; calibration
  and test March-June 2007
MSR ship to ISRO, August 2007
I&T at ISAC, August 2007-July
  2008


                                     4
Getting Ready to Go




                      5
Launch and Mission




                     6
Some First Results




                     7
Moon Minerals and Particles




                              8
Mini-SAR Experiment Objectives

Map the deposits of both poles of
  the Moon (> 80° lat.) at optimum
  viewing angles (~40°) to
  characterize permanently dark
  areas and definitively determine
  their RF backscattering
  properties using both SAR and
  scatterometry
Complete the global map of the
  Moon by mapping dark regions
  in lunar polar areas
Characterize the physical nature of
  the polar regolith and surface
SAR mapping of other targets of            Moon South Pole
                                      Clementine 750 nm base map
  opportunity as possible


                                                                   9
Circular Polarization Ratio (CPR)

Ratio of received power in both
    right and left senses
Normal rocky planet surfaces =
    polarization inversion (receive
    opposite sense from that
    transmitted)
“Same sense” received indicates
    something unusual:
      double- or even-multiple-
          bounce reflections
      Volume scattering from RF-
          transparent material
High CPR (enhanced “same
    sense” reception) is common
    for fresh, rough (at
    wavelength scale) targets and
    water ice



                                                 10
MSR Coverage from First Mapping Cycle




                                        11
180˚

                                         Plaskett




                                                               Haskin

                            Rozhdestvensky




    Lovelace

                                              Whipple                      Nansen
90˚ W                   Hermite                                              90˚ E
                                                  Peary

        Sylvester
                                     88˚ N




                           84˚ N              Byrd



                                         Gloja
                                                      Main L   De Sitter
                80˚ N
                                             0˚                                      12
North Polar CPR Map




                      13
A Tale of Two Scatterers




                  Main L   14
15
16
180˚

                                         Plaskett




                                                                   Haskin

                            Rozhdestvensky




    Lovelace


                                              Whipple                          Nansen
90˚ W                   Hermite                                                  90˚ E

                                                  Peary
        Sylvester
                                     88˚ N




                           84˚ N              Byrd



                                         Gloja

                                                          Main L   De Sitter
                80˚ N
                                             0˚                                          17
180˚




  Fresh craters




Anomalous craters


                    90˚ W                            90˚ E



                                            88˚ N




                                    84˚ N




                            80˚ N
                                               0˚            18
Water Equivalent Hydrogen (wt.%)




                                   19
Summary
Mini-SAR successfully mapped about 90% of both polar
  areas; due to some operational issues, coverage is
  not contiguous
Calibration data from Earth and Moon have been
  acquired and partly processed; used to quantify radar
  response
Non-polar areas analyzed; results consistent with
  previous S-band radar mapping from Earth
Areas of high CPR have been identified:
   Some high CPR is clearly associated with surface roughness
     (e.g., Main L ejecta blanket)
   Some deposits (e.g., near north pole on floor of Peary) show
     high CPR and are restricted to the interior of craters; these
     features are in permanent darkness.


                                                                     20
Some Lessons Learned

Sensitivities about ITAR
  US must recognize that foreign institutions may view
    ITAR restrictions negatively
  Foreign governments must realize that wording is
    not chosen by the flight partners
  ITAR issues did not materially interfere with MSR
    build, test, and operation
  ITAR compliance is simply an overhead lien that
    must be paid


                                                     21
Some Lessons Learned

Interactions with the press
  Other governments may have different relationships
    with press
  Keep quiet and let your lead partner set the tone
  “No comment” is a comment; it will not deter a
    determined reporter




                                                   22
Project Management Practices
          for Indian Space Vehicles




                        Dr. BN Suresh
Director, Indian Institute of Space Science and Technology,
       (Former Director, Vikram Sarabhai Space Centre)
                  Thiruvananthapuram, India.



                                                              Used with Permission
ISRO Launch Vehicle Evolution

                                                                       GSLV Mk III
                                                                           March 2011

                                                             GSLV

                                             PSLV

                          ASLV

   SLV-3




Launch Vehicle      SLV            ASLV             PSLV        GSLV           GSLV Mk III
Lift-off weight
      (kg)          17              40              295          450              635
 Payload (kg)     40 (LEO)       150 (LEO)      1800 (SSO)    2200 (GTO)       4000 (GTO)
Management Structure
                           (For Launch Vehicle Programmes)

 A Core Project team with overall                             Matrix Management Structure
  responsibility
                                                                    Project Director
 System Projects in new / critical areas
                                                                    Asso. Project Director
 Distributed work environment (work
  centers all over India)                                        System            Project Directors
                                                                  System
                                                                 Projects
                                                                    System
 New technology development at ISRO units                        Projects
                                                                      System       System Projects
                                                                    Projects
                                                                       System
 Large scale facility build-up                                       Projects
                                                                       Projects
     Launch complex, Propulsion systems development,




                                                                                              Development
                                                                                                Agencies
      testing, Avionics systems and Vehicle level testing               Dy. Project
      & mock ups etc.                                                    Directors
 Large scale industrial production
     Motor cases, Light alloy structures & Propellant tanks         Project Managers
      Liquid / Cryo engine systems, Avionics system                 for various systems
      components, Propellants & chemicals, Sub
      assemblies integration etc.
 Implementation of change & configuration
                                                                     Project Engineers
  control
Core Project Responsibilities
Responsibilities of the Core Project have been :


 Definition and implementation of project management plan &
  procedures.
 Communication of project objectives and plans to all levels
 Mission specification & interfaces with users.
 Launch complex and tracking network interfaces.
 Vehicle systems definition and specifications.
 Stage engineering and interfaces control.
 Vehicle / stage level configuration control & change management
 Direct monitoring of progress in all key areas
 Speedy execution without compromising performance and
  quality
 Programme management, cost/schedule monitoring and control.
 Organise project related reviews at micro and macro levels
Programme Control Cycle
           Used in Development

                    • Generated programme plans,
Establishing          system development plans,
  Targets             schedules & milestone plans.


 Monitoring         • Monitored through weekly
                      biweekly and monthly review
Performance           meetings, progress reports.


Programme            • Compared actual progress with
  Analysis             expected performance.



Management           • Identified solution options,
                       implemented decisions & follow
 Reporting             up of needed actions.
Techno- Managerial Review Mechanisms
     Management of Scope, Time & Cost without compromising Quality

 Project Review Meetings
        Weekly review of project activity status

 Project Executive Reviews (PEX) : Tier - 1
                                                                                Scope



        Monthly reviews for resolving technical / managerial issues          Quality

 Reviews by Centre Director
                                                                       Time             Cost
        Technical / managerial

 Reviews by Project Management Boards (PMB) : Tier - 2
        General guidelines, budget approvals, schedules, facility & manpower

 Reviews by Project Management Council (PMC) : Tier - 3
        Overall policy guidelines

 Reviews by Chairman, ISRO
        Technical / managerial
Technical Review Milestones followed
                                     Preliminary                              Objectives are closely tracked
                           System      Design
                           Concept                                              In all milestone reviews.
                                       Review              Critical
                           Review                          Design
                                         PDR
                            SCR                            Review       Test
                                                            CDR       Readiness
    Normalised work load




                                                                       Review       System
                                                                        TRR        Readiness
                                                                                    Review
                                                                                      SRR


                                     Time in years                                    6-7 years


Objectives SCR                                       PDR                    CDR                      SRR

 System configuration.                   Technical adequacy of       Approval of specs.      Detailed interface
 System /subsystem                         design approach             and design.             performance checks.
  specs.                                  Firm up specs. for          Approval of baseline  Certify system
 Manufacturing & test                      system / subsystems         production              performance meets
  facilities.                             Physical and functional     Firm up interfaces      requirements
 Schedule & resource                       interfaces definition.     Firm up detailed test  Finalise system
  projections                             Clearance for detailed       plan                    configuration
                                            design.                                            Approval for7 system
                                                                                                commissioning
Overall Management Approach



Managing Technical         Schedule
      Risks               Management


             Launch Vehicle
                Project
              Management


Quality management      New Technology
 Cost Management         Development
Managing Technical Risks
The following procedures are strictly implemented.

   Identification of single point failure

   Redundancy management for mission critical Avionics / Control systems
   Vendor directory /Preferred part list

   Well evolved part screening for electronic components

   Process documents & QA / QC plans

   Test & evaluation at different levels

   Integrated system level checks

   Detailed simulations at different levels

   FMECA analysis /Fault tree analysis
Project Schedule Management
   Optimal sharing of resources between numerous operational and
    development programmes
   The following methodologies are strictly implemented throughout the
    Project phase
                     Work Break down Structures (WBS)
                   Schedule analysis (PERT/CPM) & simulations
                   Identifying ‘limiting factors’
                   Anticipating criticalities
Time management
                   ‘Feed forward’ control– Real time correction of plans
                      as work progresses, Work around plans
                   Fast tracking through Concurrent Engineering approach
                   Near critical paths & criticality index
                   Integrated Information network for faster communication
Management Information System used

                                Data Input                     From Work centres




                            Analysis/Processing                   By Project




                                                                 To Management
                            Information/Output



      For decision making                     For progress monitoring



Project Executives & Management         Participating Agencies, Centre level
             Forums                                   Forums
Quality Management
 Key processes and continuous Quality control during development
  and realisation of all launch vehicle subsytems are identified and
  carried out.
 The Strict Quality Assurance is ensured by meticulously following the
  various steps given below.
        Approved specifications & design
        Qualified materials, Process reviews
        Inspection/Surveillance during production
        Stage clearances                             Quality              Quality
        3 tier non conformance management           Assurance             Control
        Batch testing for VOQ, Acceptance testing

 The Quality Audit is given utmost importance
        Using appropriate equipments
                                                                 Quality
        Reference Standards                                      Audit
        Monitoring of key characteristics
        Maintenance of records & traceability
        Verification through audits
Project Cost Management
 Cost Estimation and Control
   The costs of the resources needed to complete project activities including
    infrastructure are worked out.
   More than 2000 line items with individual line item code for each launch
    vehicle project are identified to define the clear cut responsibilities
   Methodologies adopted for cost control
          Maximal use of available technologies, proven designs
          Planning for contingencies & cost escalations in the initial stage itself
          Standardization & stock piling standard parts in the beginning
          Design for manufacture (DFM) & concurrent engineering methodologies.
          Taking calculated risks - Realization of subsystems in numbers based on confidence
           in design / analysis without waiting for test results
          Optimal hardware rotation plan for different test programme
          Optimal sequencing of number of tests & test durations
          ‘Make or buy’ decisions with focus on ‘comparative advantage’

                                                                   S Curve
 Expenditure Control Methodologies
    Through Periodic management reviews
    Changes through department approved re-
     appropriation procedures & approval cycles
    S-Curve analysis for schedule/cost
Managing Technology
      Developments


                                                                                                           Larger engines
                                                                                                              in future
                                                                                  Indigenous 20 ton
                                                                                 Cryo engine by 2010

                                                  Indigenous 7.5/ 9
                                                  ton Cryo engine
                                                  (2008)

                                GK Cryo
                                (Russian)
 Adopt available technologies or near term                             One gigantic leap may lead to failure
  technologies
 Step by step approach for new technology
                                                    Learning level



  development. Manageable learning steps.
 Identification of key improvement packages                                                   Feasible size jumps
  in terms of performance, reliability & cost &
  provide thrust for development
 Identification of key strategic areas for                          Initial level
  indigenization – e.g. Cryogenic technology
  strategic materials                                                                     Time
Change Management

 Control of intersystem interfaces has been the major
  responsibility of the project team.
 The evolution and changes in the design are continuously
  monitored and the impacts assessed.
 Traceability of changes, decisions and inputs are utilised to
  assess the impacts of a new change.
 Design changes and requirements are closely monitored during
  development and changes are meticulously catalogued.
 Dissemination of the information across the system teams are
  done expeditiously using management information tools.
 Management of changes is given high priority to ensure the
  success of operational launches.
Launch Campaign Management
                  •   Launch vehicle
Integrated Team   •   Space craft
                  •   Propellant servicing / Safety
     Effort
                  •   Tracking & ground station
                  •   Logistics

                  •   Mission Director
  Campaign        •   Vehicle Director
 management       •   Satellite Director
   system         •   Range Director
                                                           Countdown
                  • Micro level scheduling on day to day   45 to 60 days
                    & hourly basis                          activity at
  Planning        • Orchestrated effort for resource        Sriharikota
 methodology        deployment
                  • More than 100 people involved per
                    launch at different phases of time

                  • Technical /progress reviews
                  • Stage clearances
   Reviews        • Authorization reviews for launch
                    Mission Readiness Review, Launch
                    Authorization Board
Conclusions. (Success through Team effort)
  The Management Structure which is in vogue has been very effective .
  The Programme Control Cycle and the Overall Management approach have
   been very efficient , leading to successful space launches.
  Indian Space ia able to implement programmes with shoe string budget
   through effective Schedule and Cost controls.
  Focus has always been on achievement of collective results.
  Time tested review mechanisms have helped to achieve technical excellence.
  Some of the key factors for the effective management of Indian Space
   Programme are:
        Engaging the teams into productive, constructive discussions around ideas and
         issues
        Accepting and committing to decisions & plan of actions arrived at by the team.
        Each identified team member is accountable for delivery as per the decided
         plans.
        Creative leadership, rewards and recognitions to the deserving team member/s
         who make significant contributions.
Source: Patrick Lencioni, The Five dysfunctions of a Team- A Leadership Fable; 2006

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Inter approach to_spaceprogmgmt

  • 1. Project Management: Brazilian Experience Himilcon de Castro Carvalho, AEB Used with Permission
  • 2. “Classic” Project Phasing & Planning 1 yr 2-3 yrs ECSS or ISO
  • 3. Reality Activity or $$ 1-2 yr 2-3 yr 4-6 yr Lack of: Budget Human Resources Infrastructure decision mobilization peak launch & ops
  • 4. Reality Activity or $$ 1-2 yr 2-3 yr 4-6 yr Lack of: Budget Human Resources Infrastructure decision mobilization peak launch & Gov't Changes ops Political OK! Economical crisis talks Let's go Changes in priorities
  • 5. Reality What was expected Activity or $$ 1-2 yr 2-3 yr 4-6 yr Lack of: Budget Human Resources Infrastructure decision mobilization peak launch & Govn't Changes ops Political OK! Economical crisis talks Let's go! Changes in priorities
  • 6. Project Organization Strong Matrix Structure (80' – 90') Mech. Electr.. Ground AIT QA ... Eng. Eng. Segment Project Office Project Office = Management + Systems Engineering QA, AIT, Ground Seg. completely dedicated to this single project
  • 7. Project Organization Weak Matrix Structure (90' – 00') Systems Mech. Electr.. Ground AIT QA ... Eng. Eng. Eng. Segment Project Office 1 Project Office 2 Project Office 3 Competition for project resources, human resources and budget
  • 8. Planning Scope Scope Schedule WBS Planning Definition Devel. Risk Mgt. Cost HR Activity Activity Plan Estimating Planning Definition Resources Risk Cost Identification Budgeting Activity Activity Sequencing Duration Qualit. Quality Risk An. Planning Quant. Comm. Risk An. Planning Risk Resp. Plan Purch. Plan Planning & Acq. Contracting
  • 9. “out of control” variables Planning “under relative control” variables Scope Scope Schedule WBS Planning Definition Devel. Risk Mgt. Cost HR Activity Activity Plan Estimating Planning Definition Resources Risk Cost Identification Budgeting Activity Activity Sequencing Duration Qualit. Quality Risk An. Planning Quant. Comm. Risk An. Planning Risk Resp. Plan Purch. Plan Planning & Acq. Contracting
  • 10. “out of control” variables Planning “under relative control” variables and focus Scope Scope Schedule WBS Planning Definition Devel. Risk Mgt. Cost HR Activity Activity Plan Estimating Planning Definition Resources Risk Cost Identification Budgeting Activity Activity Sequencing Duration Qualit. Quality Risk An. Planning Quant. Comm. Risk An. Planning Risk Resp. Plan Purch. Plan Planning & Acq. Contracting
  • 11. Impacts PM under severe HR and Budget Restrictions  Low responsivity  Schedules not used as actual management tool  Small number of concurrent projects  Low industry dynamics  Focus on WBS  Focus on Activity Definition & Sequencing  Focus on Quality/Verification Planning  Special focus on Risk Planning
  • 12. Thank you! Himilcon de Castro Carvalho Director of Space Policy and Strategic Investments Brazilian Space Agency himilcon@aeb.gov.br
  • 13. Mini-SAR An Imaging Radar on India’s Chandrayaan-1 Mission to the Moon Paul D. Spudis MSR Principal Investigator Lunar and Planetary Institute Houston TX spudis@lpi.usra.edu www.spudislunarresources.com NASA Program Management Challenge 2010 February 2010 1
  • 14. Origins Waikaloa, Hawaii 2003 Dr. Narendra Bhandari talk on proposed Chandrayaan-1 mission (not yet selected for flight) I approach him to fly radar; he encourages it APL submits unsolicited letter proposal ISRO decides on open competition for foreign payloads (< 10 kg, < 100 W), Feb. 2004 Submit formal proposal, April 2004 Selected for flight, September 2004 2
  • 15. Approval Getting the money from NASA Technology interest from SOMD; exploration interest from ESMD Technology development package developed and jointly funded Getting approval from Dept. of State Present instrument concept/overview to DoS Dec. 2004 Formal application for export license Jan. 2005 State approval June 2005 Getting final approval from ISRO TAA draft sent to ISRO in June 2005; no response Continuous delay; demand for change of title of TAA document TAA signed during May 2006 India visit by M. Griffin (NASA Administrator) 3
  • 16. Build and test Mini-SAR (re-named Mini-RF) gets underway May 2005; instrument PDR Dec. 2005 Chandrayaan/MSR ICD draft written and approved Nov. 2005 Mini-SAR CDR Sept. 2006 Chandrayaan-1 CDR May 2007 Mini-SAR ship to APL; calibration and test March-June 2007 MSR ship to ISRO, August 2007 I&T at ISAC, August 2007-July 2008 4
  • 20. Moon Minerals and Particles 8
  • 21. Mini-SAR Experiment Objectives Map the deposits of both poles of the Moon (> 80° lat.) at optimum viewing angles (~40°) to characterize permanently dark areas and definitively determine their RF backscattering properties using both SAR and scatterometry Complete the global map of the Moon by mapping dark regions in lunar polar areas Characterize the physical nature of the polar regolith and surface SAR mapping of other targets of Moon South Pole Clementine 750 nm base map opportunity as possible 9
  • 22. Circular Polarization Ratio (CPR) Ratio of received power in both right and left senses Normal rocky planet surfaces = polarization inversion (receive opposite sense from that transmitted) “Same sense” received indicates something unusual: double- or even-multiple- bounce reflections Volume scattering from RF- transparent material High CPR (enhanced “same sense” reception) is common for fresh, rough (at wavelength scale) targets and water ice 10
  • 23. MSR Coverage from First Mapping Cycle 11
  • 24. 180˚ Plaskett Haskin Rozhdestvensky Lovelace Whipple Nansen 90˚ W Hermite 90˚ E Peary Sylvester 88˚ N 84˚ N Byrd Gloja Main L De Sitter 80˚ N 0˚ 12
  • 25. North Polar CPR Map 13
  • 26. A Tale of Two Scatterers Main L 14
  • 27. 15
  • 28. 16
  • 29. 180˚ Plaskett Haskin Rozhdestvensky Lovelace Whipple Nansen 90˚ W Hermite 90˚ E Peary Sylvester 88˚ N 84˚ N Byrd Gloja Main L De Sitter 80˚ N 0˚ 17
  • 30. 180˚ Fresh craters Anomalous craters 90˚ W 90˚ E 88˚ N 84˚ N 80˚ N 0˚ 18
  • 32. Summary Mini-SAR successfully mapped about 90% of both polar areas; due to some operational issues, coverage is not contiguous Calibration data from Earth and Moon have been acquired and partly processed; used to quantify radar response Non-polar areas analyzed; results consistent with previous S-band radar mapping from Earth Areas of high CPR have been identified: Some high CPR is clearly associated with surface roughness (e.g., Main L ejecta blanket) Some deposits (e.g., near north pole on floor of Peary) show high CPR and are restricted to the interior of craters; these features are in permanent darkness. 20
  • 33. Some Lessons Learned Sensitivities about ITAR US must recognize that foreign institutions may view ITAR restrictions negatively Foreign governments must realize that wording is not chosen by the flight partners ITAR issues did not materially interfere with MSR build, test, and operation ITAR compliance is simply an overhead lien that must be paid 21
  • 34. Some Lessons Learned Interactions with the press Other governments may have different relationships with press Keep quiet and let your lead partner set the tone “No comment” is a comment; it will not deter a determined reporter 22
  • 35. Project Management Practices for Indian Space Vehicles Dr. BN Suresh Director, Indian Institute of Space Science and Technology, (Former Director, Vikram Sarabhai Space Centre) Thiruvananthapuram, India. Used with Permission
  • 36. ISRO Launch Vehicle Evolution GSLV Mk III March 2011 GSLV PSLV ASLV SLV-3 Launch Vehicle SLV ASLV PSLV GSLV GSLV Mk III Lift-off weight (kg) 17 40 295 450 635 Payload (kg) 40 (LEO) 150 (LEO) 1800 (SSO) 2200 (GTO) 4000 (GTO)
  • 37. Management Structure (For Launch Vehicle Programmes)  A Core Project team with overall Matrix Management Structure responsibility Project Director  System Projects in new / critical areas Asso. Project Director  Distributed work environment (work centers all over India) System Project Directors System Projects System  New technology development at ISRO units Projects System System Projects Projects System  Large scale facility build-up Projects Projects  Launch complex, Propulsion systems development, Development Agencies testing, Avionics systems and Vehicle level testing Dy. Project & mock ups etc. Directors  Large scale industrial production  Motor cases, Light alloy structures & Propellant tanks Project Managers Liquid / Cryo engine systems, Avionics system for various systems components, Propellants & chemicals, Sub assemblies integration etc.  Implementation of change & configuration Project Engineers control
  • 38. Core Project Responsibilities Responsibilities of the Core Project have been :  Definition and implementation of project management plan & procedures.  Communication of project objectives and plans to all levels  Mission specification & interfaces with users.  Launch complex and tracking network interfaces.  Vehicle systems definition and specifications.  Stage engineering and interfaces control.  Vehicle / stage level configuration control & change management  Direct monitoring of progress in all key areas  Speedy execution without compromising performance and quality  Programme management, cost/schedule monitoring and control.  Organise project related reviews at micro and macro levels
  • 39. Programme Control Cycle Used in Development • Generated programme plans, Establishing system development plans, Targets schedules & milestone plans. Monitoring • Monitored through weekly biweekly and monthly review Performance meetings, progress reports. Programme • Compared actual progress with Analysis expected performance. Management • Identified solution options, implemented decisions & follow Reporting up of needed actions.
  • 40. Techno- Managerial Review Mechanisms Management of Scope, Time & Cost without compromising Quality  Project Review Meetings  Weekly review of project activity status  Project Executive Reviews (PEX) : Tier - 1 Scope  Monthly reviews for resolving technical / managerial issues Quality  Reviews by Centre Director Time Cost  Technical / managerial  Reviews by Project Management Boards (PMB) : Tier - 2  General guidelines, budget approvals, schedules, facility & manpower  Reviews by Project Management Council (PMC) : Tier - 3  Overall policy guidelines  Reviews by Chairman, ISRO  Technical / managerial
  • 41. Technical Review Milestones followed Preliminary Objectives are closely tracked System Design Concept In all milestone reviews. Review Critical Review Design PDR SCR Review Test CDR Readiness Normalised work load Review System TRR Readiness Review SRR Time in years 6-7 years Objectives SCR PDR CDR SRR  System configuration.  Technical adequacy of  Approval of specs.  Detailed interface  System /subsystem design approach and design. performance checks. specs.  Firm up specs. for  Approval of baseline  Certify system  Manufacturing & test system / subsystems production performance meets facilities.  Physical and functional  Firm up interfaces requirements  Schedule & resource interfaces definition.  Firm up detailed test  Finalise system projections  Clearance for detailed plan configuration design.  Approval for7 system commissioning
  • 42. Overall Management Approach Managing Technical Schedule Risks Management Launch Vehicle Project Management Quality management New Technology Cost Management Development
  • 43. Managing Technical Risks The following procedures are strictly implemented.  Identification of single point failure  Redundancy management for mission critical Avionics / Control systems  Vendor directory /Preferred part list  Well evolved part screening for electronic components  Process documents & QA / QC plans  Test & evaluation at different levels  Integrated system level checks  Detailed simulations at different levels  FMECA analysis /Fault tree analysis
  • 44. Project Schedule Management  Optimal sharing of resources between numerous operational and development programmes  The following methodologies are strictly implemented throughout the Project phase  Work Break down Structures (WBS)  Schedule analysis (PERT/CPM) & simulations  Identifying ‘limiting factors’  Anticipating criticalities Time management  ‘Feed forward’ control– Real time correction of plans as work progresses, Work around plans  Fast tracking through Concurrent Engineering approach  Near critical paths & criticality index  Integrated Information network for faster communication
  • 45. Management Information System used Data Input From Work centres Analysis/Processing By Project To Management Information/Output For decision making For progress monitoring Project Executives & Management Participating Agencies, Centre level Forums Forums
  • 46. Quality Management  Key processes and continuous Quality control during development and realisation of all launch vehicle subsytems are identified and carried out.  The Strict Quality Assurance is ensured by meticulously following the various steps given below.  Approved specifications & design  Qualified materials, Process reviews  Inspection/Surveillance during production  Stage clearances Quality Quality  3 tier non conformance management Assurance Control  Batch testing for VOQ, Acceptance testing  The Quality Audit is given utmost importance  Using appropriate equipments Quality  Reference Standards Audit  Monitoring of key characteristics  Maintenance of records & traceability  Verification through audits
  • 47. Project Cost Management  Cost Estimation and Control  The costs of the resources needed to complete project activities including infrastructure are worked out.  More than 2000 line items with individual line item code for each launch vehicle project are identified to define the clear cut responsibilities  Methodologies adopted for cost control  Maximal use of available technologies, proven designs  Planning for contingencies & cost escalations in the initial stage itself  Standardization & stock piling standard parts in the beginning  Design for manufacture (DFM) & concurrent engineering methodologies.  Taking calculated risks - Realization of subsystems in numbers based on confidence in design / analysis without waiting for test results  Optimal hardware rotation plan for different test programme  Optimal sequencing of number of tests & test durations  ‘Make or buy’ decisions with focus on ‘comparative advantage’ S Curve  Expenditure Control Methodologies  Through Periodic management reviews  Changes through department approved re- appropriation procedures & approval cycles  S-Curve analysis for schedule/cost
  • 48. Managing Technology Developments Larger engines in future Indigenous 20 ton Cryo engine by 2010 Indigenous 7.5/ 9 ton Cryo engine (2008) GK Cryo (Russian)  Adopt available technologies or near term One gigantic leap may lead to failure technologies  Step by step approach for new technology Learning level development. Manageable learning steps.  Identification of key improvement packages Feasible size jumps in terms of performance, reliability & cost & provide thrust for development  Identification of key strategic areas for Initial level indigenization – e.g. Cryogenic technology strategic materials Time
  • 49. Change Management  Control of intersystem interfaces has been the major responsibility of the project team.  The evolution and changes in the design are continuously monitored and the impacts assessed.  Traceability of changes, decisions and inputs are utilised to assess the impacts of a new change.  Design changes and requirements are closely monitored during development and changes are meticulously catalogued.  Dissemination of the information across the system teams are done expeditiously using management information tools.  Management of changes is given high priority to ensure the success of operational launches.
  • 50. Launch Campaign Management • Launch vehicle Integrated Team • Space craft • Propellant servicing / Safety Effort • Tracking & ground station • Logistics • Mission Director Campaign • Vehicle Director management • Satellite Director system • Range Director Countdown • Micro level scheduling on day to day 45 to 60 days & hourly basis activity at Planning • Orchestrated effort for resource Sriharikota methodology deployment • More than 100 people involved per launch at different phases of time • Technical /progress reviews • Stage clearances Reviews • Authorization reviews for launch Mission Readiness Review, Launch Authorization Board
  • 51. Conclusions. (Success through Team effort)  The Management Structure which is in vogue has been very effective .  The Programme Control Cycle and the Overall Management approach have been very efficient , leading to successful space launches.  Indian Space ia able to implement programmes with shoe string budget through effective Schedule and Cost controls.  Focus has always been on achievement of collective results.  Time tested review mechanisms have helped to achieve technical excellence.  Some of the key factors for the effective management of Indian Space Programme are:  Engaging the teams into productive, constructive discussions around ideas and issues  Accepting and committing to decisions & plan of actions arrived at by the team.  Each identified team member is accountable for delivery as per the decided plans.  Creative leadership, rewards and recognitions to the deserving team member/s who make significant contributions. Source: Patrick Lencioni, The Five dysfunctions of a Team- A Leadership Fable; 2006