ARES III Industry Day Minutes-Attendees-Slides.pdf
PDF 5 MB Posted
- Solicitation number
- FA9300-11-R-0002
View the file
Other files
Show all 29
On GovTribe
Work with this file
- Download the original file
- Contacts named in this file
- Similar government files
- Ask GovTribe AI about this file
Text version
Advanced Research and Engineeringand Engineering
Services Industry Day
9 May 2011 Contracting Officer - Teresa Weber, AFFTC/PKT
Program Manager - Jamie Malak, AFRL/RZSE
PA Case # 11123 Distribution A: Approved for public release; unlimited distribution
Attachment 2 – Industry Day Slides
Agenda
• 7:30 to 8:30 – Meet and Greet Social
• 8:30 to 9:15 – Opening Remarks and Introductions
Sh Philli AFRL/RZS– Shawn Phillips, AFRL/RZS
– Richard Cohn, AFRL/RZSE
• 9:15 to 9:45 – Contractual Overview
• 9:45 to 10:00 – Break
• 10:00 to 10:30 – Technical Overview
• 10:30 to 11:00 Q & A• 10:30 to 11:00 – Q & A
• 11:00 to 1:00 – Lunch
• 11:30 to 4:00 – Individual Sessions
Industry Day
• Advanced Research & Engineering Services (ARES) OverviewOverview
– Provide on-site Research and Engineering Services
• Early Industry Involvement
– Encourage competition
– Feedback from industry
GOVERNMENT TEAM
POC’s
• Procuring Contract Officer
– Teresa L Weber teresa weber@edwards af mil 661-277-2101– Teresa L. Weber, teresa.weber@edwards.af.mil 661-277-2101
• Contract Specialists
– Aimee Buckless, aimee.buckless@edwards.af.mil 661-277-1992@
– Tom Shea, thomas.shea@edwards.af.mil 661-277-8592
• Source Selection Lead
– Richard Cohn, richard.cohn@edwards.af.mil 661-275-6177
• Project Manager
– Jamie Malak, jamie.malak@edwards.af.mil 661-275-5539
Space & Missile Division
Shawn PhillipsS a ps
Air Force Research Laboratory, Propulsion DirectoratePropulsion Directorate, Space & Missile Division Deputy Chief
Air Force Research LaboratoryAir Force Research Laboratory Ed d Ai F B CAEd d Ai F B CAEdwards Air Force Base, CAEdwards Air Force Base, CA
ARES Industry DayARES Industry DayARES Industry DayARES Industry Day 9 May 20119 May 2011
Dr. Shawn PhillipsDr. Shawn Phillips Deputy ChiefDeputy Chief
Space & Missile Propulsion DivisionSpace & Missile Propulsion Division shawn.phillips@edwards.af.milshawn.phillips@edwards.af.mil
Distribution A: Approved for release to DoD and their Contractors only
Air Force Materiel Command
MISSION
Deliver war-winningDeliver war-winning ...
- Technology
- Acquisition
- Test
S- Sustainment ... expeditionary capabilities to the warfighter
AFMC Units cover R&D Lab, Product Centers, Test Centers, Sustainment Centers
Air Force Research Laboratory
Mission: Leading the discovery, development and integration of affordable warfighting f technologies for America's aerospace forces.
AFRL People & Facilities
• 10 Major R&D sites across US
• 40 Locations around the World
10 T h i l Di t t• 10 Technical Directorates
• Air Vehicles (RB)
• Directed Energy (RD)
• Human Effectiveness (RH) (711 HP Wing)
• 5,400 Gov’t Employees
• Information (RI)
• Space Vehicles (RV)
• Munitions (RW)
• Materials & Manufacturing (RX)
, p y
• 3,800 On-site Contractors g ( )
• Sensors (RY)
• Propulsion (RZ)
• AF Office of Scientific Research (AFOSR)
AFRL Propulsion Directorate
(AFRL/RZ)
Create and Transition Propulsion and Power Technology f Milit D i f Ai d S
Space & MissileSpace & MissileSpace & MissileSpace & Missile HypersonicsHypersonicsHypersonicsHypersonics for Military Dominance of Air and Space
Space & Missile Space & Missile PropulsionPropulsion
Space & Missile Space & Missile PropulsionPropulsion
HypersonicsHypersonicsHypersonicsHypersonics
Turbine EnginesTurbine EnginesTurbine EnginesTurbine Engines
Energy, Power & Energy, Power & ThermalThermal
Energy, Power & Energy, Power & ThermalThermal
Propulsion & Power are Important!
40-70% of cruise missile weight; the critical factor in survivability, lethality, & reach
50-70% of satellite weight 25-40% of system cost the lifesystem cost the life-limiting factor
45-80% of directed
70-90% of launch weight 40-60% of t t energy weapon weight and volume system cost
60-80% of tactical missile weight the critical factor in range & time-to-target
40-60% of aircraft
TOGW 20-40%
of system life cycle cost Air Force fuel costs were $6B in FY07 alone
10Distribution A: Approved for public release; unlimited distribution
AFRL Propulsion Directorate
RZ-East (Wright Patterson AFB OH)
RZ-West (Edwards AFB CA)
( g t atte so O )
Turbine Engines Ramjet Engines Combined-Cycle Engines
Rocket Engines & Motors Satellite Propulsion Advanced Propulsion
Hypersonic Engines Aircraft Power Thermal Management
Fuels and Propellants System Analysis
Fuels and Propellants System Analysis
“RZ-West” Organization
RZ
Propulsion Directorate
MR. DOUG BOWERS
INTEGRATION & OPS
DIVISION (WEST)
RZO (Deputy)
FINANCE BRANCH
(WEST)
RZFB
SPACE & MISSILE
PROPULSION DIVISION
ASSOC DIRECTOR
SITE COMMANDER
RZSRZ
DET 7
5-5620
MR. K. VANDERDHYDE MRS. RUTH DECOY
BUSINESS
OPERATIONS
MR. TJ TURNER
RZOF
RZOI
CHIEF OF SAFETY
MS DEB FULLER
SE
EXECUTIVE OFFICER
2 d LT E i Mill
CCE
MR. MIKE HUGGINS
AEROPHYSICS
DR. INGRID WYSONG
RZSA
RZSP
EXPERIMENTAL DEMO
MS. JULIE CARLILE
RZSO
SITE COMMANDER
COL MIKE PLATT
INFORMATION
TECHNOLOGY
MR. CARL OUSLEY
RZOIMS. DEB FULLER
QUALITY ASSURANCE
TSGT TIMOTHY ROWE
QA
2nd LT Eric Miller
MOTORS
CAPT SETH MAREK
ENGINES
DR. RICH COHN
PROPELLANTS
CAPT TRE DOBSON
RZSP
SPACECRAFT
DR. JAMES HAAS
RZSS
CONTRACTS
AFFTC/PKT
RZSB
RZSE
MATERIALS APPS
MAJ VINCE PEL
RZSM
PAYOFF STUDIES
MR. ROY HILTON
RZST
MS. LUCY CASTEL
RZ (Edwards)Det 7 Other As of: 1 JAn 11
AFRL at Edwards AFB
MOJAVEMOJAVE
BORONBORONHWY 58HWY 58
E R
O A
D E
R O
A
D HWY 58HWY 58
R O
C K
ET
S
IT
E
R O
C K
ET
S
IT
E
EDWARDS AIR FORCE BASEEDWARDS AIR FORCE BASE Air Force Research
Laboratory
ROGERSROGERS
DRY LAKEDRY LAKE
AFFTCAFFTC
R
B
LV
D
R B
LV
D
RESERVATION BOUNDARYRESERVATION BOUNDARY
HWY 395HWY 395
ROSAMOND BLVD.ROSAMOND BLVD.
MERCURY BLVD.MERCURY BLVD.
Laboratory Site
ROSAMONDROSAMOND
AVENUE EAVENUE E
H
IG
H W
A Y
H
IG
H
W A
Y
LA
N
C A
ST
ER
LA
N
C A
ST
ER
ET
E
A
ST
ET
E
A
ST
RESERVATION BOUNDARYRESERVATION BOUNDARY
SCALE IN MILESSCALE IN MILES
ROSAMONDROSAMOND
DRY LAKEDRY LAKE
LANCASTERLANCASTER 14
0t h
ST
R
EE
0t h
ST
R
EE 0 5 10
Air Force Research Laboratory Edwards AFB Propulsion Directorate Facilities
1-56 HIGH THRUST COMPLEX
1-52 ROCKET MOTOR ENGINE COMPLEX
1-46
CHEMICAL HANDLING RESEARCH FACILITY
1-42
SPACE ENVIRONMENT PROPULSION COMPLEX
LIQUID PROPELLANT STORAGE
1-38
ENVIRONMENT
1-36
MOTOR
X-33 LAUNCH SITE
LIQUID PROPELLANT STORAGE
GUARD
POST
2-20 GENERAL
SUPPORT AREA
2-10
FABRICATION AREA
STORAGE
COMPLEX
BEHAVIOR
COMPLEX
1-32
MOTOR
COMPONENT
COMPLEX
1-30
PROPELLANT/
COMPONENT
SILO
COMPLEX
SCIENCE, ENGINEERING,
AND DATA CENTER
ELECTRIC PROPULSION
LABORATORY
SOLAR PROPULSION
FACILITY
PHYSICAL
SCIENCE
LABORATORY
COMPLEX
2-15 MATERIEL
CENTER 1-60
COMPLEX
1-90
SATELLITE TEST
AND INTEGRATION
FACILITY
NATIONAL HOVER
TEST FACILITY
LABORATORY1-21
PROPELLANT
PREPARATION
LABORATORY
1-14
SATELLITE
PROPULSION
COMPLEX
TITAN SRM
TEST FACILITY
TS-1C1-125
1-120 1-115
LARGE
HYDROCARBON
1-40
PROPELLANT
STORABILITY
COMPLEX
LARGE ENGINE/COMPONENT
TEST FACILITY
TS-1A
TEST FACILITY
TS-1D
Edwards Site: Unique Capability
• 65 Square Mile Development Test Facility
Air quality constraints do not inhibit testing– Air quality constraints do not inhibit testing
– Noise abatement not a problem
– Wind/population corridor does not inhibit testing
– Environmental monitor/control systems in place
– Flight Test Center relation/support ongoing
• 135 Major Lab/Engineering Facilities & Buildings
• 30 Major Active Test Areas/Stands
– Unique geophysical set-up ($2 5B+ investment)Unique geophysical set-up ($2.5B+ investment)
15Distribution A: Approved for public release; unlimited distribution
Facilities
Bench-level Labs High Thrust Facilities
• 19 Liquid Engine stands, up to
8,000,000 lbs thrust
• 13 Solid Rocket Motor pads, up to
10 000 000 lbs thrust10,000,000 lbs thrust Altitude Facilities
• From micro-newtons to
50,000 lbs thrust50,000 lbs thrust
16Distribution A: Approved for public release; unlimited distribution
History
• 1939 – Rocket research begins at Power Plant Lab, Wright Field OH
• 1947 Edwards AFB selected for rocket testing• 1947 – Edwards AFB selected for rocket testing
• 1959 – Rocket scientists move from WPAFB to Edwards
• 1997 – AF labs consolidated into AFRL
• Key Accomplishments
– Saturn V F-1 engine development
– Minuteman ICBM silo basing
– XLR-129 engine (for Shuttle main engine)
– Peacekeeper ICBM developmentPeacekeeper ICBM development
– Missile defense interceptor HOVER tests
– Titan IV solid rocket motor upgrade
– RS-68 engine for Delta IV EELV
Resources: People
CIVIL SERVICE Total M.S. Ph.D.
Scientists and Engineers 104 16 47 Technicians 20 0 0 Administrative 29 1 0 CO-OPs 9 1 0 Student Support (S.T.E.P., etc..) 7 0 0 Palace Acquire 1 0 0
TOTAL CIVIL SERVICE 170 18 47
CONTRACTORS Total M.S. Ph.D.
Scientists and Engineers 90 19 14 Technicians 90 2 0 Administrative 101 2 0
TOTAL CONTRACTORS 281 23 14
OTHER Total M S Ph DOTHER Total M.S. Ph.D.
Intergovernmental Personnel 0 0 0
18As of: 9-Nov-09 RZ-WestDistribution A – Public release, unlimited distribution
Resources: People
ACTIVE-DUTY MILITARY Total M.S. Ph.D.
Scientists and Engineers 44 7 1 Technicians 8 0 0 Pgm mgrs/Admin 1 1 0
TOTAL ACTIVE DUTY MILITARY 53 8 0
IMAs Total M.S. Ph.D.
Scientists and Engineers 3 1 1 Technicians 2 0 0
TOTAL IMAs 5 1 1
19As of: 9-Nov-09 RZ-WestDistribution A – Public release, unlimited distribution
RZ-West People
Military (65)
Civil Service (175)
On-site Contractors
(240)
Advanced Degrees 13% PhD
11% MS
11% MS
PR-West Functional Layout
Finance
Experimental Demonstration
Engines Motors Spacecraft
Propulsion Materials Applications Applications and Assessments
Aerophysics Propellants
Integration and Operations Distribution A – Public release, unlimited distribution. Release Number: PA07385A
Integrated High Payoff Rocket Propulsion Technology (IHPRPT)
Joint government and industry effort focused on developing affordable technologies for revolutionary, reusable and/or rapid response military global reach capability sustainable strategicresponse military global reach capability, sustainable strategic missiles, long life or increased maneuverability spacecraft capability and high performance tactical missile capability
ELVsELVs ICBMsICBMs MicroMicro--SatellitesSatellites
SMV/SOVSMV/SOV
High Energy High Energy Upper StagesUpper Stages
SLBMsSLBMs SatellitesSatellites
AirAir--toto--Air MissilesAir Missiles Ground/SurfaceGround/Surface Launched MissilesLaunched Missiles
Space and Missile R&D Building Block Process
6.1 6.2 6.3
23Distribution A: Approved for public release; unlimited distribution
Branch Expertise
• RZSA – Aerophysics
– Characterize, model, and analyze propulsion fluid and energy flow
• RZST – Payoff Studies
– Provide unbiased analysis and assessment from component levelp p gy processes
– Non-equilibrium flows, combustion devices, plumes assessment from component level through system level in support of internal and external customers
• RZSB – Motors
• RZSP – Propellants
– Liquid, solid rocket propellant modeling, synthesis, h t i ti & d l t
S oto s
– Exploratory and Advanced development of solid propulsion technologies characterization, & development
• RZSM – Materials Applications
– Basic & Exploratory research into application of materials to rocket
• RZSE – Engines
– Exploratory and Advanced development of liquid rocket engine application of materials to rocket propulsion components
– Areas of research: High Temperature Components, Polymers, Propellant Fracture technologies
• RZSS – Spacecraft
– Exploratory and Advanced y , p Mechanics
• RZSO – Experimental Demonstrations (test facilities) p y development of spacecraft propulsion technologies
Distribution A – Public release, unlimited distribution
Current R&D Thrusts
Hydrocarbon Boost
Multi-mode Satellite Propulsion
Advanced Solid Motors
Upper Stage Engine Tech
“Green” Monopropellants
All-electric Orbit Transfer
Questions?
26Distribution A: Approved for public release; unlimited distribution
Source Selection Lead
Richard Cohnc a d Co
Air Force Research Laboratory, Propulsion DirectoratePropulsion Directorate, Engine Branch Chief, Source Selection Lead
Contract History
• 20+ Year History (first contract started in 1987) Scientific Engineering and Technical Assistance (SETA)– Scientific Engineering and Technical Assistance (SETA)
– 2001 Name Changed to ARES
• ARES I and ARES IIARES I and ARES II
– Small Business competitive source selections
W t ARES III t b i il• We expect ARES III to be similar
– A final determination has not been made
• Don’t believe rumors!
Meeting Objectives
• Objectives of Industry Day
– Present proposed program: clarify acquisition strategy, goals, and schedule
– Provide details on Request For Proposals (RFP)Provide details on Request For Proposals (RFP)
– Gain concurrence/feedback from industry on this plan.
– Feedback required by 22 Mayq y y
• Email feedback to teresa.weber@edwards.af.mil and thomas.shea@edwards.af.mil
– Q & A responses will be posted under FA9300-11-R-0002 inQ & A responses will be posted under FA9300-11-R-0002 in FEDBIZOPPS NLT 27 May 2011
Business Overview
Contracting OfficerContracting Officer
Teresa L. Weber
Contracting Overview
• Current Contract
• Requirements to do Business with the GovernmentRequirements to do Business with the Government
• Acquisition Background
• Contract Type
• Contract Structure
• Acquisition Conditions
• Oversights
• Deliverables
• Tentative Contracting Milestones• Tentative Contracting Milestones
• Base Support/Government Furnished Services
• Organizational Conflict of Interest
Distribution A: Approved for public release; unlimited distribution g
• Source Selection
Current Contract
• ARES II
• Current Contractor: Jackson and Tull
• Contract Type: CPFF
• Original Basic Contract Value: $14.9M
• Current Contract Value/Option: $29.8 M
• NAICS Code: 541710 - Research and Development in the Physical, Engineering, and Life Sciences
- 1000 Employees
Requirements to do Business with the Government
• Central Contractor Registration (CCR) required in accordance with FAR
4.1102. Access at: http://www.ccr.gov/.
• Online Representations and Certifications(ORCA): is an e-Government initiative that has been developed to replace most of the paper basedinitiative that has been developed to replace most of the paper based Representations and Certifications (Reps and Certs) process, known as Section K, an internet application that allows user access 24/7.
Access at: http://orca.bpn.gov
• Wide Area Work Flow(WAWF): Contractors will submit payment requests in accordance with the instructions contained in their specificrequests in accordance with the instructions contained in their specific contract. Reference DFARS 252.232-7003. Contact your particular DCMA office for training. Access at: https://wawf.eb.mil/
Acquisition Background
• Project Name: ARES III
• On Site Support – AFRL/RZ- West
• Period of Performance: 2 Year Basic
2 Year Option 1
1 Year Option 2
Total 5 Year Contract
Estimated Total Contract: $24.7M
Tentative Contract Type
• Cost-Plus-Fixed-Fee + Performance Incentive
– CPFF (3%)+ PI (4%)
• Performance Incentive Criteria
– Management
– Technical
– Cost
– Schedule
Performance Incentive Criteria
• Management
– Five % max personnel overdue on mandatory Air Force training– Five % max. personnel overdue on mandatory Air Force training
– Zero security violations
• Technical
– All employee meet or exceed all position requirements
• Cost
– Travel vouchers contain no unallowable charges
– Submitted vouchers contain no more than 2 error greater than $25 each per six month periodp p
– Wrap rate as define by the government ≤ proposed wrap rate
Performance Incentive Criteria
• Schedule
– Contractor to identify qualified perspective candidates within 30 days– Contractor to identify qualified perspective candidates within 30 days of receipt of any new requirement
– All reports received on-time per SOW and CDRLs, none overdue by more than 5 daysmore than 5 days
– Invoices submitted on-time, none overdue by more than 5 days
Performance Incentive Percentages
Period 1 Period 2 Period 3 Period 4 Percent of incentive pool paid at end of
0 5 0 5 0 5 0 5evaluation period 0.5 0.5 0.5 0.5
Percent of incentive pool deferred to end of contract 0.5 0.5 0.5 0.5
Contract Structure
• Basic contract R&D CLIN structure
– CLIN 0001 Phase In (FFP)
– CLIN 0002 ARES Prime Labor (CPFF + PI)
– CLIN 0003 ARES Subcontracts (CPFF + PI)– CLIN 0003 ARES Subcontracts (CPFF + PI)
– CLIN 0004 Reimbursables (Cost)
– CLIN 0005 DD250 Data (NSP)
– CLIN 0006 Non DD250 Data (NSP)
• Option Periods R&D CLIN structure
– CLIN X002 ARES Prime Labor (CPFF + PI)CLIN X002 ARES Prime Labor (CPFF + PI)
– CLIN X003 ARES Subcontracts (CPFF + PI)
– CLIN X004 Reimbursables (Cost)
Acquisition Conditions
• Conditions that may be considered for contract performance
– Security classification
– Base support
– Organizational Conflict of Interest
(OCI)
– International Traffic in Arms Regulations (ITAR)
– Public Law 98-94 (Export Control)
– Non Disclosure Agreements (NDA)
– Associate Contractor Agreements
(ACA)Public Law 98 94 (Export Control)
– Computer security requirements
– No foreign participation
– Unlimited data rights
– Environmental and safety requirementsg
– Hazardous materials
Oversight
• Management In-House Reviews
R l d t t G t P M• Regular updates to Government Program Manager and Task Manager
• Performance Incentive Reviews (every six• Performance Incentive Reviews (every six months)
• Invoice ReviewInvoice Review
Deliverables
• Monthly Funds and Man-Hour Expenditure Report
C t t F d St t R t• Contract Funds Status Report
• Technical Reports – Contract Status & Mgmt ReportReport
• Property Control Plan
• State Environmental Health and Safety Plan
• Quarterly Progress Reports
• Scientific and Technical Final Report
• Software
Organizational Conflict of Interest
• Per AFFARS 5352.209-9000 P t fli ti l hi h bi th– Prevents conflicting roles which may bias the contractor’s judgment of objectivity, or to preclude the contractor from obtaining an unfair fcompetitive advantage in concurrent or future acquisitions.
– Alt III – May not use other company’s proprietaryAlt III – May not use other company s proprietary information in any other way or purpose
– Alt VI – Restrictions are binding to any g y subcontractors – prime must include in any subcontracts Both Alts apply to this contract
– Both Alts apply to this contract
Tentative Contracting Milestone
• RFP release Jul 2011
• Proposals due (45 days) Aug 2011
• Proposal evaluation Sep 2011
• Contract Award Jan 2012
• Phase- In (30 days) Mar 2012( y )
• Full Performance Apr 2012
Base Support
• Office space, furniture, telephones, computers
• Emergency medical treatment
• Security police support
• Firefighter support
Source Selection
• Award based on Best Value
E l ti f t• Evaluation factors
• Factor 1: Mission Capability
• Technical scenarios
• Program management
• Subcontract management
Personnel Recruitment and retention plan• Personnel Recruitment and retention plan
• Factor 2: Past Performance
• Factor 3: Cost/Price
• Factor 1 is most important. Factors 2 and 3 are equal in importance and of lesser importance than Factor 1.
• Factor 1 >(Factor 2 = Factor 3)
• Factor 1 >(Factor 2 = Factor 3)
Source Selection
• Written & Electronic Proposals
Electronic spreadsheets must include formulas
• Oral Presentations
• 15 minutes company description/capabilitiesp y p p
• 45 minutes evaluated
• Factor 1, subfactors 2, 3 and 4
Technical Overview
Program ManagerProgram Manager
Jamie Malak
Technical Overview
• Current Demographics
• R h A• Research Areas
• Contract Management
S /• Security / ITAR Restrictions
Current Demographics
Current*
• E i 16 Present Degree Breakdown
PhD 2• Engineers 16
• Technicians 3
• PhD 2
• MS 3
• Mgmt/Admin 4 • BS/BA 12
• Aerospace Engineering 4
• Chemical Engineering 1
• Mechanical Engineering 9
C S i 1
*Does not include contract management
• Computer Science 1
• Math 1
• Technical Writing 1
Technical Writing 1
Technology Areas
• General Technology Areas
– Liquid Propulsion Technology
– Solid Propulsion Technology
– Emerging and Pervasive Technology
– Spacecraft Propulsion Technologygy
– Systems Integration and Analysis
Liquid Propulsion Technology
• Goal: Development of technology for liquid rocket engines and propulsion systems
• Technology Activities:
Analytical codes Injector designsInjector designs Combustion devices and nozzle designs Turbomachinery designs
• Liquid rocket engine control & condition monitoring systems
• Materials applications
• Reliability and failure analysesReliability and failure analyses
• Tankage, feed systems and advanced materials applicable to storable, cryogenic and high pressure systems Comparisons of liquid propulsion system components
Comparisons of liquid propulsion system components
Liquid Propulsion Technology
• Example of current task:
– Modeling jets in a cross-flow within a supercritical regime.Modeling jets in a cross flow within a supercritical regime.
Solid Propulsion Technology
• Goals: Development of technologies for solid and hybrid rocket motors
• Technology Activities:
Performance, cost, reliability, hazards, failure, andPerformance, cost, reliability, hazards, failure, and technology transition impacts
– Advanced solid and hybrid rocket motor technologiesy g
Development
–ModificationModification
–Fabrication
T ti
–Testing
Solid Propulsion Technology
– Gathering qualitative behavioral and quantitative data pertaining to the particle impingement and deposit on exit cone.
Emerging and Pervasive Technology
• Goals: applied sciences and technologies of boost, post-boost satellite and kinetic energy weaponspost-boost, satellite and kinetic energy weapons systems
• Technology activities:Technology activities:
Advanced propulsion concepts
• Formulation of propellant ingredients• Formulation of propellant ingredients
• Hazard evaluation
• Structural and aging properties of propellant
Emerging and Pervasive Technology
• Example of current task:
Providing engineering support designing and constructing– Providing engineering support designing and constructing Acoustic High Pressure Cryogenic Chamber.
Spacecraft Propulsion Technology
• Goal: Support spacecraft applications (satellite, post boost vehicle and kinetic energy weapon programs, etc)gy p p g )
• Technology activities:
– Computerized analytical capabilities
– Component and integrated system design
– Mission analyses with current and planned axial and divert propulsion programspropulsion programs
– Design, analysis, testing of kinetic energy weapons
– Thermal analysis and combustion modelingThermal analysis and combustion modeling
– Generic spacecraft propulsion systems engineering support
– Staging and separation event software algorithms
Distribution A: Approved for public release; unlimited distribution
Staging and separation event software algorithms development, launch vehicle integration
Systems Integration and Analysis
• Goal: competing performance concepts and subsystems (avionics, sensors, and propulsion for ballistic missiles, space transportation t t )systems, etc)
• Technology activities:
Performance requirements and figures of meritPerformance requirements and figures of merit
• Database augmentation
Analysis tools Competing propulsion systems investigation
• Planning processes and activities support
• Exhaust plume radiation signature prediction
Sensitivity analysis
• Literature reviews
• Literature reviews
Systems Integration and Analysis
– Plume dispersion analysis for on-site large scale testingPlume dispersion analysis for on site large scale testing.
Contract Management
• Goal: Technical and funds management, WBS planning and WBS managementmanagement
• Management activities:
Management supportg
Program management
Critical skill / experience retention
Program reviews
Quarterly reports
Software documentation and usage rights
Contract Management (cont)
• Management activities (cont):
S itSecurity
Training
Environmental Safety and Occupational HealthEnvironmental, Safety and Occupational Health
Property
Associate Contracting AgreementsAssociate Contracting Agreements
Non-Disclosure Agreements
Management Information System with the capability to g y p y identify, track, and manage task costs, budgets and invoices
Security
• Work site is in an access controlled area
– Badges required
– Military base requirements
– Special requirements for visitor access
• Some classified information is generatedg
• Vast majority of documentation produced has limited distribution
• ITAR information is generated
Security (cont.)
• ITAR (International Traffic in Arms Regulations) and EAR (Export Administration Regulations) - government’s limitation on export control and public publication and dissemination of information
• All websites, documents, briefings must be reviewed and approved by the Scientific and Technical Information Officeapproved by the Scientific and Technical Information Office (STINFO) prior to release.
• Dept of Defense, Dept of Commerce and the Dept of State have guidelines ALL must be satisfiedguidelines -- ALL must be satisfied
Security (cont.)
• Contractors have a responsibility to inform their subcontractors and commercial suppliers that they mustsubcontractors and commercial suppliers that they must also comply
• For further information, please reference:, p
• ITAR, 22 CFR 120-130,
http://www.pmdtc.org/consolidated_itar.htm
•EAR, 15 CFR 730-774,
http://www.access.gpo.gov/bis/ear/ear_data.html
Questions & DiscussionQuestions & Discussion
File details come from the government source that posted it. Updated .