space test program - cal polymstl.atl.calpoly.edu/~jfoley/spring2010/spring workshop 2010...
TRANSCRIPT
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Department of Defense
Space Test Program
“Access to Space”
2d Lt Chalie L. Galliand, USAF
Spaceflight Mission Design Manager,
Mission Design Division
Space Development &Test Wing
Office: 505-846-5329
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Agenda
• STP Overview
• SERB Process
• Reimbursable Flight Basis
• STP Access to Space
• Enablers
• Standards
• Roadmap
• Rideshare Opportunities
• Government Rideshare Working Group
• EELV Standard Service
• Summary
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DoD Space Test Program (STP)
• Chartered by OSD in 1965• First flight in 1967
• Primary provider of mission design,
s/c acquisition, integration, launch,
and on-orbit ops for DoD and DoD
sponsored space experiments,
technologies & demos• Ability to provide all spaceflight
services except the experiment itself
• Single manager for all DoD payloads
on the Space Shuttle and ISS
• Designated AFSPC’s “Front door”
for all auxiliary payloads seeking
flight opportunities on DoD missions
STP has flown STP has flown 491491 experiments on experiments on Over Over 203203 missions since 1967missions since 1967 (As of 23 Mar 10)
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Col Scott HandyCommander
SpaceTest Group
SDTW Organization
Col Michael MoranSpace Dev & Test Wing
Commander
SDTW/OMMgt Ops
SDTW/PCProgram Control
SDTW/PKContracting
Col Steve HargisCommander
SpaceDevelopment Group
Space Test Sq
Spacecraft Development Sq
Space TestOperations Sq
Launch Test Sq
Responsive Space Sq
SDTW/ENEngineering
SDTW/XPPlans & Policy
Col Jeffrey HaymondSpace Dev & Test Wing
Vice Commander
Human Spaceflight Payloads Division
MissionDesign Division
Responsive Satellite C2
Division
STP Dire
ctor
STP
Senior IMA
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Access to STP Services
• Space Experiments Review Board (SERB)
• Manifest based on:
• SERB rank
• Flight opportunities
• Mission requirements
• Available STP funds
>$10M = SAF/USA approval
<$10M = STP director approval
• Reimbursable flight basis
• Manifest based on:
• Flight opportunities
• Available manpower
• Available customer funds
• SMC/CC and HQ AFSPC approval
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Space Experiments Review Board (SERB) Process
Service & Lab SERBs
• Rank experiments
• Submit to DoD
Service & Lab SERBs
• Rank experiments
• Submit to DoD
AF AFRL
Navy
Army
DARPA
MDA
NRO
DoD SERB SAF/USA
DoD SERB• SAF/USAL chairs• Hears 15-min. brieffrom experimenter
• Multi-servicemembership
• Evaluatesmilitary relevance
• Does notevaluate funding
• Experiment may bekept off by maj. vote
DoD SERB• SAF/USAL chairs• Hears 15-min. brieffrom experimenter
• Multi-servicemembership
• Evaluatesmilitary relevance
• Does notevaluate funding
• Experiment may bekept off by maj. vote
SAF/USA• Approves SERB List• Approves missions >$10M
• AF funding viaCorporate process
• EA for DoD
SAF/USA• Approves SERB List• Approves missions >$10M
• AF funding viaCorporate process
• EA for DoD
STP• Executes mission• Approves missions <$10M • Satellite bus development• Launch• Operations (1 yr)• Shuttle/ISS ops• Does NOT fund experiments
STP• Executes mission• Approves missions <$10M • Satellite bus development• Launch• Operations (1 yr)• Shuttle/ISS ops• Does NOT fund experiments
• Experiments must address operational need
• Strategic S&T investment for DoD
• Military Relevance is 60% of DoD SERB score
STP
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SERB Annual Schedule
Notional timeline--actual dates dependant on individual organizations
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Service SERB Process
• AF10-1202, AR70-43, OPNAVINST 3913.1B provides
Space Test Program (STP) Management guidance
• Service/Organization level SERBs administered by
local directives
• Organization/Service determines: board membership, presentation requirements, scoring criteria
• Results and required documentation from service SERB provided to SAF/USA
• Air Force Coordinator: • Mr John Cao, AFRL/RVE, ABQ, 505-846-7222, [email protected]
• Navy Coordinator:• LCDR Richard Murphy, DoD STP, ABQ, 505-853-3766, [email protected]
• Army Coordinator: • Mr Stephen Cayson, USASMDC, AL, 256-955-3605, [email protected] .mil
• For all other DoD sponsors contact: • Eric Thorson, SAF/USA, Washington D.C, 713-588-7379, [email protected]
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Auxiliary Payload Process
Flight opportunity
exist?
STP drafts MOA & MRD
describing opportunity
APL is compatible
LV and/or PP conduct
Feasibility Studies
LV or PP initiates APL integration
STARTSTART
STP receives APL request & evaluates
maturity
IDs possible flight opportunities
STP submits Manifest Package
Final approval by SMC/CC & AFSPC/A3
APL Manifest Approval
Mission, Flight & Launch
Readiness Reviews
STOP
STOP
STOP
Reprinted courtesy of USAF
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Agenda
• STP Overview
• SERB Process
• Reimbursable Flight Basis
• STP Access to Space
• Enablers
• Standards
• Roadmap
• Rideshare Opportunities
• Government Rideshare Working Group
• EELV Standard Service
• Summary
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STP Access to Space
• Spaceflight Methods:• Shuttle/International Space Station (ISS)/Other NASA vehicles
• Deployable, payload bay, mid-deck lockers, ISS internal/external
• Auxiliaries• Piggybacks payloads: leverage margin on existing SC
• Secondary SC: leverage margin on existing LV
• Dedicated Launches (Minotaur, Falcon, Raptor, EELVs, sub-orbital sounding rockets)
• Also high-altitude balloons and zero-g flights
ISS
Space Shuttle
Sounding rocket
Zero G Flight Minotaur IVHigh-altitude balloon
Atlas V
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Agenda
• STP Overview
• SERB Process
• Reimbursable Flight Basis
• STP Access to Space
• Enablers
• Standards
• Roadmap
• Rideshare Opportunities
• Government Rideshare Working Group
• EELV Standard Service
• Summary
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Setting Standards through Enablers
Maximize Launch Opportunities using Standardization
• Proactive measures to standardize SC design & construction• Based on 40+ years of lessons learned
• Cohesive approach throughout space community• AFRL, ARMY, DARPA, NASA, NRL, NRO, SMC, along w/contractors and universities
• STP Enablers• EELV Secondary Payload Adapter (ESPA) CLASS SC
• Standard Interface Vehicle (SIV)• Fast Affordable Science & Technology Satellite (FASTSAT)
• Multi-Payload Adapter (MPA) - Minotaur IV• Hydrazine Auxiliary Propulsion System (HAPS) – Minotaur IV• Poly Picosatellite Orbital Deployer (P-PODs) / CubeSat
• Accommodations on multiple LVs/SVs, Space Shuttle
• Multi-Mission Space Operations Center (MMSOC) GSA
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Spaceflight Standards (“Enablers”)
SIVSIV
(Standard Interface Vehicle)• ESPA Class SC ≤ 180kg• 1-4 Experiments• Heritage subsystems• Compatible w/ multiple LVs • Compatible w/ MMSOC & AFSCN• Storable until launch identified
ESPA ESPA
(EELV Secondary Payload Adapter)• SC weight ≤ 180kg• SC Volume – 35.5” x 28” x 24”• CG Location - < 20’’ from the SSIP• Mechanical Interface – 15”• Electrical: Battery charge/monitor• Fundamental Frequency > 35hz
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HAPSHAPS
(Hydrazine Auxiliary Propulsion System)
• Dual orbits from small LVs• Precise orbit insertion• First demo - STP-S26 ILC May 10
FASTSATFASTSAT
(Fast Affordable Science & Technology)
• 6 Expts on maiden voyage (MINI-ME, TDS, MST, TTI, PISA,
Nanosail-D)• CubeSat capable • ~18 month design-to-flight ready
Spaceflight Standards (“Enablers”)
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PP--PODPOD
(Poly-Picosat Orbital Deployer)• 10x10x10 cm cube, ~ 1 kg mass
(“1U”)• Qualified LVs: Rockot, Dnepr, Minotaur I• In Development: Falcon-1, Minotaur IV
MPA MPA
(Minotaur IV Multi-PL Adapter)• Holds up to 4 ESPA Class SC• Mass ≤ 180kg• Volume – 35.5” x 28” x 24”• Maximizes lift capability• First demo - STP-S26 ILC May 10
1 U CubeSat (Cal Poly1)
Spaceflight Standards (“Enablers”)
Cal Poly P-POD
MEPSI on STSMEPSI on STS--113 (Nov 02) & STS113 (Nov 02) & STS--116 (Dec 06)116 (Dec 06)
Proximity Ops and InspectionProximity Ops and Inspection
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JEMJEM--EF, COLEF, COL--EPFEPF
(Japanese Experiment Module External Facility,
Columbus External Payload Facility)• International Partner external ISS sites• 4 JEM-EF, 2 COL-EPF available to US• Similar to ELC; JEM-EF higher mass• 30-36 month design-to-flight ready
ELCELC
(Express Logistics Carrier)• Reusable external platforms on the ISS • 8 experiment locations• 500 pounds, > 500 watts• High and Low rate data• 24 month design-to-flight ready
Spaceflight Standards (“Enablers”)
Both OperationalBoth Operational
COL-EPF
JEM-EF
ELC 1 & 2 InstalledELC 1 & 2 Installed
During STSDuring STS--129 mission129 mission
16 Nov 200916 Nov 2009
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CRSCRS
(Commercial Resupply Services)• SpaceX and Orbital Sciences Corp• Pressurized and unpressurized lift• Sample return via SpaceX Dragon• Exploring small sat deployment options
ISS ISS -- PressurizedPressurized
• Internal experiment volume• Express Rack, power and data• Human in the loop testing• 18-24 month design-to-flight ready
Spaceflight Standards (“Enablers”)
Expected to be Operational 2011Expected to be Operational 2011
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Current/Planned ISS External Payloads
MISSE 6 LWAPA(returns Mar 10)
HREP(Launched Sep 09
JEM-EF)
MISSE 7 & PRELSE(Launched Nov 09
& Jul 10 ELC#2)
STP-H3(Launches Jul 10
ELC#3) SPHERES
REBR (42P up, ATV2 down)
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NASA International Partner VehiclesNASA International Partner Vehicles
• Japanese H-IIB Transfer Vehicle• Pressurized and Unpressurized• JEM-EF & ELC payload lift• No return
• European Automated Transfer Vehicle• Pressurized payload lift• No return
• Russian Progress• Pressurized payload lift• No return
• Russian Soyuz• Primarily crew rotation• Very limited payload lift• Very limited sample return
Spaceflight Standards (“Enablers”)
All OperationalAll Operational
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STP Enablers Roadmap
FY09 FY10 FY11 FY12 FY13 FY14
EELV Stnd Svc Rides—1/yr beginning FY12
MMSOC�Standard TT&C interface
�Creates an “open system”
environment
SIV� Enables 60kg/100W
payload
� Up to 4 P/Ls per S/C
� IDIQ contract for 6
buys
Minotaur IV MPA� Up to 4 ESPA S/C
� Multiple P-POD locations
� HAPS compatible
ESPA� Proven on STP-1
� Enables up to six
400lb APLs on
EELVsSTP-M17
FASTSAT� 12 mos design-to-
build
� Cubesat capable
� Low-cost ESPA S/C
STP-S26
w/ cubesats
STP Small Launch Vehicles Minotaur I/IV, Falcon 1/1E, etc.
DSX
DMSP-19
HAPS�Multiple orbits from small
Launch Vehicles
�Precise orbit insertion
STP-S27
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STP Enablers Roadmap
• ELC 1&2; STS-129, 16Nov 09
• ELC 3; STS-134, 29 Jul 10
• ELC 4; STS-133, 16 Sep 10
8 locations, various opportunities through ISS lifetime
ELC� 8 External ISS payload
sites
� 500 lbs, 500 watts
� Various viewing
opportunities
various opportunities through ISS lifetime
various opportunities through ISS lifetime
JEM-EF and COL-EPF� 4 JEM-EF, 2 COL-EPF
� ~500lbs, 500watts
� Ram, wake, nadir, zenith
ISS - Pressurized� Express Rack, power &
data
� Human-in-the-loop
� Many unique possibilities
CRS 3CRS 2CRS 1SpaceX Demo
MissionsTBD TBD
2 – 3 missions per year
1 – 2 missions per year
HTV & ATV approx 1 msn/year, Progress and Soyuz many/yr
IP Resupply missions� Pressurized &
unpressurized
� JEM-EF and ELC rotation
CRS – Orbital Cygnus� Pressurized only
� No sample return
FY09 FY10 FY11 FY12 FY13 FY14
DemoCRS 1
TBD
TBDTBD
CRS – SpaceX Dragon� Pressurized &
unpressurized
� ELC payload rotation
� Sample return
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Agenda
• STP Overview
• SERB Process
• Reimbursable Flight Basis
• STP Access to Space
• Enablers
• Standards
• Roadmap
• Rideshare Opportunities
• Government Rideshare Working Group
• EELV Standard Service
• Summary
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• Why Rideshare?
• Dedicated launches too expensive
• Partnerships share the financial burden
• Innovation key to success
• DoD STP leads USG Rideshare Working Group
• Explores USG, commercial & foreign launch
opportunities
• Builds partnership missions
• Payloads include STP experiments
& USG Auxiliary Payloads (APL)
STP Rideshare
•• ESPA Standard ServiceESPA Standard Service
•• Standard Interface VehicleStandard Interface Vehicle
•• MM--IV MultiIV Multi--Payload AdapterPayload Adapter
•• PPODsPPODs
Kodiak Star spacecraft suite
PICOSat
PCSat
SAPPHIRE
STP-1Standardization Standardization
Reduces:Reduces:
RiskRisk
ComplexityComplexity
CostCost
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EELV Standard Service
• Expect one ESPA ring to
fly a year starting 2012
• Multiple ESPA class SC
opportunities a year
• All APLs through STP
• Various Orbits
• Cost TBD
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Agenda
• STP Overview
• SERB Process
• Reimbursable Flight Basis
• STP Access to Space
• Enablers
• Standards
• Roadmap
• Rideshare Opportunities
• Government Rideshare Working Group
• EELV Standard Service
• Summary
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Summary
• STP has a long history of creating successful
collaborative missions to provide experiments and
auxiliary payloads with access to space.
• Payloads can come to STP either via the SERB for a
subsidized flight or as a reimbursable.
• Personnel at STP are experienced and well versed at
developing creative and cost effective missions
designed to maximize government and/or customer
resources.
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QUESTIONS?