Space Test Program
Space Test Program
Space Test Program
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Department of Defense<br />
<strong>Space</strong> <strong>Test</strong> <strong>Program</strong><br />
“Access to <strong>Space</strong>”<br />
Lt Chalie Galliand, USAF<br />
<strong>Space</strong>flight Mission Design Manager,<br />
Mission Design Division<br />
<strong>Space</strong> Development &<strong>Test</strong> Directorate<br />
Office: 505-846-5329<br />
Chalie.galliand@kirtland.af.mil
Previous Activities, 1 st Year<br />
2
Previous Activies, 2 nd Year<br />
3
• STP Overview<br />
• STP Mission and History<br />
• Paths to STP support<br />
• SERB Process<br />
• APL Process<br />
• STP Access to <strong>Space</strong><br />
• Enablers<br />
• Standards<br />
• Roadmap<br />
• Rideshare Opportunities<br />
• Summary<br />
• Government Rideshare Working Group<br />
• EELV Standard Service<br />
Agenda<br />
4
• “…provide mission design, spacecraft<br />
acquisition, integration, launch, and on-orbit<br />
operations for the maximum number of<br />
DoD… experiments, consistent with priority,<br />
opportunity. and available funding.”<br />
– STP Management and Funding Policy<br />
• “The STP has been designated as the “front<br />
door” for all DoD auxiliary payloads (APLs)<br />
on DoD, civil and commercial launches, and<br />
for all non-DoD APLs seeking launch<br />
opportunities on DoD missions.”<br />
– STP AFI 10-1202; AR 70-43; OPNAVINST 3913.1B<br />
• “single manager for all DoD payloads on the<br />
<strong>Space</strong> Shuttle, the ISS, future manned and<br />
unmanned NASA launch vehicles…”<br />
– STP AFI 10-1202; AR 70-43; OPNAVINST 3913.1B<br />
The STP Mission<br />
5
PNT<br />
(NTS-1: 1974)<br />
Missile Defense<br />
(RM-15: 1967)<br />
<strong>Space</strong> Control<br />
(SOICAL-3: 1969)<br />
507 Experiments on<br />
Over 212 Missions<br />
Since 1967<br />
STP History<br />
Communications<br />
(LES 6: 1968)<br />
Weather<br />
(HiLat-1983)<br />
STP has flown and will continue to fly advanced technology leading to<br />
(As of 23 Mar 10)<br />
tomorrow’s operational systems<br />
6
C/NOFS<br />
COSMIC<br />
Coriolis<br />
From Concept to Reality<br />
DWSS<br />
COSMIC-II<br />
SSAEM<br />
Worldwide<br />
Data<br />
Usage<br />
STP is Critical to the Rapid Transitioning of Systems from Experiment<br />
to Operational Systems<br />
7
• CubeSat Proliferation<br />
CubeSats<br />
• 10 Countries have successfully deployed CubeSats<br />
• Over 250 institutions developing CubeSats, including<br />
Peru and Ecuador (Academia, Gov’t & Industry)<br />
• Growing number of STP experiments are CubeSats or<br />
CubeSat compatible payloads<br />
• 2007 DoD SERB : 4 CubeSats 2 Compatible Payloads<br />
• 2008 DoD SERB : 7 CubeSats 6 Compatible Payloads<br />
• 2009 DoD SERB: 8 CubeSats 5 Compatible Payloads<br />
• 2010 DoD SERB: 10 CubeSats 7 Compatible Payload<br />
• CubeSat Potential<br />
• Potential for operational use in many mission areas<br />
• SSA, SEM, ISR, and COMM<br />
• Several DoD agencies working to build operational<br />
missions<br />
9
• CubeSats on STP Launches<br />
Directorate CubeSat Activities<br />
• Previously Launched: MEPSI, PSSC, GeneSat, PharmaSat<br />
• Missions On-Orbit:<br />
• STP-S26: RAX, O/OREOS, Nanosail-D<br />
• Missions selected for Manifest on CRS:<br />
• Tethersat, BK-1, SMDC-TechSat, GROUP-C, PSSC <strong>Test</strong>bed,<br />
TEPCE<br />
• SDTO developing CubeSat Ground System<br />
• Funded by SMC/XR & STP<br />
• SENSE is first mission with G/S having residual capabilities for<br />
future AF CubeSat mission<br />
• Collaborating with SMC/XR on SENSE project<br />
• 2 SSAEM CubeSats<br />
• SMC/SD to launch and operate<br />
• STP participating member in the CubeSat Standards Committee<br />
• Working to develop standard integration practices and procedures<br />
10
Number of SERB CubeSats<br />
11
STP CubeSat Manifest Process<br />
STP-2 ESPA SS STP-S27 CRS<br />
STP IS<br />
AUX PAYLOAD<br />
INTERFACE<br />
RAMPART PSat BK1 GROUP-C<br />
STP CubeSat Queue<br />
ISS<br />
NPS-CL<br />
12
Access to STP Services<br />
• <strong>Space</strong> Experiments Review Board (SERB)<br />
• Manifest based on:<br />
• SERB rank<br />
• Flight opportunities<br />
• Mission requirements<br />
• Available STP funds<br />
>$10M = SAF/AQS approval<br />
AF<br />
AFRL<br />
Navy<br />
Army<br />
Others<br />
Service & Lab SERBs<br />
• Rank experiments<br />
• Submit to DoD<br />
<strong>Space</strong> Experiments Review Board<br />
(SERB) Process<br />
• Experiments must address operational need<br />
• Strategic S&T investment for DoD<br />
• Military Relevance is 50% of DoD SERB score<br />
DoD SERB SAF/AQS<br />
DoD SERB<br />
• SAF/AQS chairs<br />
• Hears 15-min. brief<br />
from experimenter<br />
• Multi-service<br />
membership<br />
• Evaluates<br />
military relevance<br />
• Does not<br />
evaluate funding<br />
• Experiment may be<br />
kept off by maj. vote<br />
SAF/AQS<br />
• Approves SERB List<br />
• Approves missions<br />
>$10M<br />
• AF funding via<br />
Corporate process<br />
• EA for DoD <strong>Space</strong><br />
STP<br />
STP<br />
• Executes mission<br />
• Approves missions
AFRL SERB<br />
Navy SERB<br />
AF SERB<br />
ARMY SERB<br />
DoD SERB<br />
SERB List<br />
SERB Annual Schedule<br />
Jan Feb Mar Apr May Jun Jul Aug Sept Oct Nov Dec<br />
Mid<br />
SERB<br />
X<br />
X<br />
X<br />
X<br />
X X<br />
Notional timeline--actual dates dependant on individual organizations<br />
15
Service SERB Process<br />
• AFI10-1202, AR70-43, OPNAVINST 3913.1B provides<br />
<strong>Space</strong> <strong>Test</strong> <strong>Program</strong> (STP) Management guidance<br />
• Service/Organization level SERBs administered by<br />
local directives<br />
• Organization/Service determines: board membership, presentation<br />
requirements, scoring criteria<br />
• Results and required documentation from service SERB provided<br />
to SAF/AQS<br />
• Air Force Coordinator:<br />
• Mr John Cao, AFRL/RVE, ABQ, 505-846-7222, john.cao@kirtland.af.mil<br />
• Navy Coordinator:<br />
• LCDR Richard Murphy, DoD STP, ABQ, 505-853-3766, richard.murphy@kirtland.af.mil<br />
• Army Coordinator:<br />
• Ms Karen O’Connor, USA ASA ALT, 703-617-0447, karen.oconnor4@us.army.mil<br />
• For all other DoD sponsors contact:<br />
• Dr Andrew Birnbaum, SAF/AQS, Washington D.C, 713-588-7379, andrew.birnbaum@pentagon.af.mil<br />
16
SERB<br />
Reimbursable<br />
Rideshare<br />
Path to STP Support<br />
Design Mission<br />
and Implement<br />
Manifest<br />
Process<br />
Design<br />
Mission and<br />
Provide ROM<br />
ID Shared Roles<br />
and<br />
Responsibilities<br />
Executable<br />
STP Mission<br />
Executable<br />
Reimbursable<br />
Mission<br />
Executable<br />
Rideshare<br />
18
STP Access to <strong>Space</strong><br />
• <strong>Space</strong>flight Methods:<br />
• Dedicated Launches<br />
• ELVs, sub-orbital sounding rockets, high-altitude balloons, zero-g<br />
flights<br />
• Shuttle/International <strong>Space</strong> Station (ISS)/Other NASA vehicles<br />
• Deployables, payload bay, mid-deck lockers, ISS internal/external<br />
• Auxiliaries<br />
• Piggyback payloads: Margin on existing SC<br />
• Secondary SC: Margin on existing LV<br />
Atlas V<br />
<strong>Space</strong> Shuttle<br />
Zero G Flight<br />
ISS<br />
High-altitude balloon<br />
Sounding rocket<br />
Minotaur IV<br />
19
Setting Standards through Enablers<br />
• Proactive measures to standardize SC design & construction<br />
• Based on 40+ years of lessons learned<br />
• Cohesive approach throughout space community<br />
• AFRL, ARMY, DARPA, NASA, NRL, NRO, SMC, along w/contractors and<br />
universities<br />
• STP Enablers<br />
• EELV Secondary Payload Adapter (ESPA) CLASS SC<br />
• Standard Interface Vehicle (SIV)<br />
• Fast Affordable Science & Technology Satellite (FASTSAT)<br />
• Multi-Payload Adapter (MPA) - Minotaur IV<br />
• Hydrazine Auxiliary Propulsion System (HAPS) – Minotaur IV<br />
• Poly Picosatellite Orbital Deployer (P-PODs) / CubeSat<br />
• Accommodations on multiple LVs/SVs, <strong>Space</strong> Shuttle<br />
• Multi-Mission <strong>Space</strong> Operations Center (MMSOC) GSA<br />
Maximize Launch Opportunities using Standardization<br />
20
ESPA<br />
(EELV Secondary Payload Adapter)<br />
• SC weight ≤ 180kg<br />
• SC Volume – 35.5” x 28” x 24”<br />
• CG Location - < 20’’ from the SSIP<br />
• Mechanical Interface – 15”<br />
• Electrical: Battery charge/monitor<br />
• Fundamental Frequency > 35hz<br />
SIV<br />
(Standard Interface Vehicle)<br />
• ESPA Class SC ≤ 180kg<br />
• 1-4 Experiments<br />
• Heritage subsystems<br />
• Compatible w/ multiple LVs<br />
• Compatible w/ MMSOC & AFSCN<br />
• Storable until launch identified<br />
<strong>Space</strong>flight Standards (“Enablers”)<br />
21
FASTSAT: Fast Affordable Science &<br />
Technology SATellite<br />
(FASTSAT-HSV01)<br />
•Flight of up-to 6 SERB experiments<br />
•Sponsor: NASA MSFC<br />
•Size: 30” x 27” x 41” tall<br />
•Mass: 328 lbs<br />
MPA<br />
(Minotaur IV Multi-PL Adapter)<br />
• Holds up to 4 ESPA Class SC<br />
• Mass ≤ 180kg<br />
• Volume – 35.5” x 28” x 24”<br />
• Maximizes lift capability<br />
• First demo - STP-S26 ILC May 10<br />
<strong>Space</strong>flight Standards (“Enablers”)<br />
22
Minotaur I<br />
Minotaur IV<br />
ESPA-Class Satellite<br />
Launch Vehicle Compatibility<br />
EELV Medium<br />
(Atlas and Delta) ESPA<br />
PEGASUS<br />
Maximize launch opportunities using 180 kg satellites & secondary<br />
adapters<br />
23
HAPS<br />
(Hydrazine Auxiliary Propulsion<br />
System)<br />
• Dual orbits from small LVs<br />
• Precise orbit insertion<br />
• First demo - STP-S26<br />
Launched 19 Nov 2010<br />
<strong>Space</strong>flight Standards (“Enablers”)<br />
CubeSat Deployers<br />
10x10x10 cm cube, ~ 1 kg mass (“1U”)<br />
• LVs: Minotaur I, Minotaur IV, Falcon-9,<br />
Rockot, Dnepr, ISS<br />
NASA Ames Deployer<br />
(6U)<br />
1 U<br />
CubeSat<br />
(Cal Poly1)<br />
Cal Poly P-POD<br />
P-POD on Minotaur I<br />
24
ELC<br />
(Express Logistics Carrier)<br />
• Reusable external platforms on the ISS<br />
• 8 experiment locations<br />
• 500 pounds, > 500 watts<br />
• High and Low rate data<br />
• 24 month design-to-flight ready<br />
<strong>Space</strong>flight Standards (“Enablers”)<br />
JEM-EF, COL-EPF<br />
(Japanese Experiment Module External Facility,<br />
Columbus External Payload Facility)<br />
• International Partner external ISS sites<br />
• 4 JEM-EF, 2 COL-EPF available to US<br />
• Similar to ELC; JEM-EF higher mass<br />
• 30-36 month design-to-flight ready<br />
ELC 1 & 2 Installed<br />
During STS-129 mission<br />
16 Nov 2009<br />
JEM-EF<br />
Both Operational<br />
COL-EPF 25
ISS - Pressurized<br />
• Internal experiment volume<br />
• Express Rack, power and data<br />
• Human in the loop testing<br />
• 18-24 month design-to-flight ready<br />
CRS<br />
(Commercial Resupply Services)<br />
• <strong>Space</strong>X and Orbital Sciences Corp<br />
• Pressurized and unpressurized lift<br />
• Sample return via <strong>Space</strong>X Dragon<br />
• Exploring small sat deployment options<br />
<strong>Space</strong>flight Standards (“Enablers”)<br />
26
Nadir/Star ELC-4<br />
(to be installed on<br />
STS-133)<br />
Current/Planned ISS External Payloads<br />
Zenith/Star ELC #2<br />
- MISSE-7 (return Feb 11)<br />
- MISSE-8 (up Feb 11)<br />
ESP-3<br />
AMS<br />
US Lab<br />
- REBR ( 2 up on HTV-2)<br />
-- REBR-1 down on HTV-2<br />
-- REBR-2 down on ATV-2<br />
Columbus EPF<br />
- MISSE 6 LWAPA<br />
(return Nov 10)<br />
ISS Flying<br />
Towards you<br />
Zenith/Port ELC-3<br />
- STP-H3 (Feb 11)<br />
JEM-EF<br />
- HREP (up Sep 09)<br />
Nadir/Port ELC-1<br />
Expanding ISS Capabilities for Use by DoD/NASA Agencies<br />
27<br />
27
NASA International Partner Vehicles<br />
• Japanese H-IIB Transfer Vehicle<br />
• Pressurized and Unpressurized<br />
• JEM-EF & ELC payload lift<br />
• No return<br />
• European Automated Transfer Vehicle<br />
• Pressurized payload lift<br />
• No return<br />
• Russian Progress<br />
• Pressurized payload lift<br />
• No return<br />
• Russian Soyuz<br />
• Primarily crew rotation<br />
• Very limited payload lift<br />
• Very limited sample return<br />
<strong>Space</strong>flight Standards (“Enablers”)<br />
All Operational<br />
28
Standards<br />
Explores Launch<br />
Opportunities:<br />
• USG<br />
• Commercial<br />
• Foreign<br />
Dedicated Launches are<br />
too Expensive<br />
Why Rideshare?<br />
Innovation is Key to Success<br />
• ESPA Standard Service<br />
• Standard Interface Vehicle<br />
• M-IV Multi-Payload Adapter<br />
• PPODs<br />
STP Rideshare<br />
DoD STP leads USG Rideshare Working Group<br />
Builds<br />
Partnership<br />
Missions<br />
Partnerships Share Cost<br />
Burden<br />
PCSat<br />
Sapphire<br />
Reduces:<br />
• Risk<br />
• Complexity<br />
• Cost<br />
StarShine<br />
PICOSat<br />
Kodiak Star spacecraft suite<br />
29
• One ESPA ring to fly a<br />
year starting 2012<br />
• Multiple ESPA class SC<br />
opportunities a year<br />
• All APLs through STP<br />
• Various Orbits<br />
• Cost TBD<br />
EELV Standard Service<br />
30
Summary<br />
• STP has a history of creating successful<br />
collaborative missions to provide experiments and<br />
auxiliary payloads with access to space.<br />
• Personnel at STP are experienced at developing<br />
creative and cost effective missions designed to<br />
maximize government and customer resources.<br />
• Access to STP services either through the SERB<br />
process or as a funded reimbursable.<br />
31
QUESTIONS?<br />
32
Backups<br />
33
• Chartered by OSD in 1965<br />
• First flight in 1967<br />
DoD <strong>Space</strong> <strong>Test</strong> <strong>Program</strong> (STP)<br />
• Primary provider of mission design,<br />
s/c acquisition, integration, launch,<br />
and on-orbit ops for DoD and DoD<br />
sponsored space experiments,<br />
technologies & demos<br />
• Ability to provide all spaceflight<br />
services except the experiment itself<br />
• Single manager for all DoD payloads<br />
on the <strong>Space</strong> Shuttle and ISS<br />
• Designated AFSPC’s “Front door”<br />
for all auxiliary payloads seeking<br />
flight opportunities on DoD missions<br />
STP has flown 507 experiments on<br />
Over 212 missions since 1967 (As of 4 April 11)<br />
34
Advocacy<br />
35
Operational Utility<br />
HICO WindSat<br />
Haiti<br />
Jan 2010<br />
ARTEMIS (TacSat-3)<br />
National Mall<br />
Washington, DC<br />
Hurricane Karl<br />
Sept 2010<br />
36
S&T STP<br />
STP Impact to Operations<br />
Operational<br />
System<br />
“Technology developed in S&T or procured from industry or other sources shall have been<br />
demonstrated in a relevant environment or, preferably, in an operational environment to be<br />
considered mature enough to use for product development.” - DoDI 5000.02<br />
“The project shall exit the Technology Development Phase when … the technology and<br />
manufacturing processes for that program or increment have been assessed and<br />
demonstrated in a relevant environment …” - DoDI 5000.02<br />
Advanced RaDeC<br />
(Operational)<br />
SAVE<br />
(Risk Reduction<br />
Experiment)<br />
SABRS<br />
(Operational)<br />
STP can support TRL-4 to TRL-6/7 development<br />
37
Launch<br />
Technology<br />
<strong>Space</strong><br />
Vehicles<br />
STP is THE Enabler of<br />
Responsive <strong>Space</strong><br />
ESPA M-IV MPA M-IV HAPS Human <strong>Space</strong> Flt<br />
On-Orbit<br />
Reprogrammable<br />
Processor<br />
CFE<br />
RAMPART<br />
Rapid Prototype<br />
<strong>Space</strong>craft<br />
Advanced<br />
Materials<br />
SIV FASTSat CubeSats<br />
MISSE<br />
38
Outreach<br />
39
Initial Mission<br />
Planning<br />
• Requirements<br />
Definition<br />
• Mission Design<br />
• Rideshare<br />
Opportunities<br />
STP Areas of Expertise:<br />
Mission Planning and Execution<br />
System<br />
Engineering and<br />
<strong>Program</strong><br />
Management<br />
45 Years Experience<br />
• SV/LV 212 Selection Missions<br />
507 Experiments<br />
• Contract Initiation<br />
• Execution through all<br />
And phases Counting…<br />
of program<br />
SC Acquisition<br />
• Active Contract for SIV<br />
• Access to other SV<br />
Contracts<br />
• Experienced Team<br />
Launch Support<br />
• Contracts executed<br />
through SDL or NASA<br />
• Rideshare with Gov or<br />
Commercial Partners<br />
Operations<br />
• <strong>Test</strong>ing through onorbit<br />
ops all in-house<br />
• Rapid transition to<br />
Operations through<br />
RSC and SOC 11<br />
All phases of mission planning, acquisition, execution, and operations<br />
can be conducted exclusively within STP or SMC/SD<br />
40
Small<br />
Satellites<br />
Medium to<br />
Large SC<br />
STP Areas of Expertise:<br />
Access To Multiple <strong>Space</strong> Vehicles<br />
STPSat-2<br />
SIV FASTSat CubeSats<br />
C/NOFS<br />
Custom <strong>Space</strong>craft<br />
FalconSat-5<br />
Academy/<br />
University<br />
Coriolis<br />
Access To Multiple<br />
Contract Vehicles<br />
STP has experience with all sizes and complexity of space missions<br />
41
STP-Standard Interface Vehicle (SIV)<br />
Overview<br />
Small SC:<br />
• ESPA class (
STP Areas of Expertise:<br />
Launch<br />
Expendable Launch Human <strong>Space</strong> Flight<br />
ESPA-SS<br />
CubeSat<br />
Deployers<br />
M-IV MPA<br />
HAPS<br />
Sub-Orbital<br />
JEM EF<br />
CRS<br />
ExPA<br />
HTV<br />
Soyuz<br />
International<br />
Launch<br />
STP’s experience and access to spaceflight enablers allow for<br />
responsive and cost effective launch solutions<br />
ATV<br />
43
Orbital Express<br />
• Complex on-orbit<br />
rendezvous and prox ops<br />
STP Areas of Expertise:<br />
Operations<br />
C/NOFS<br />
• 1 year experimental ops<br />
transitioned to provide<br />
operational data<br />
• Data now used by<br />
multiple gov/mil<br />
agencies<br />
STPSat-2<br />
• Acquisition Team<br />
Participates in Ops<br />
Rehearsals<br />
• SCA held by STP Director<br />
• Ground Station Developed<br />
in SMC/SD<br />
SMC/SD has the unique capability of allowing responsive, in-house<br />
access to the SC operators<br />
44
Interagency<br />
CloudSat<br />
• History of cooperative<br />
satellite ops with NASA<br />
and other gov agencies<br />
STP Areas of Expertise:<br />
Operations<br />
CubeSats<br />
• In-house CubeSat ops<br />
capability in work<br />
• Access to multiple<br />
ground station options<br />
End-to-End Support<br />
• Acquisition Team<br />
Participates in Ops<br />
Rehearsals<br />
• SCA held by STP<br />
Director<br />
• Ground Station<br />
Developed in SMC/SD<br />
SMC/SD has the unique capability of allowing responsive, in-house<br />
access to the SC operators<br />
45
Government<br />
Rideshare<br />
• STP can forge bonds<br />
across multiple Gov<br />
organizations<br />
STP Areas of Expertise:<br />
Rideshare<br />
DoD Rideshare<br />
• SERB experiments<br />
can augment/increase<br />
the operational<br />
capability for<br />
low or no cost<br />
Commercial<br />
Rideshare<br />
API on AEHF<br />
CMEWS on NASA STEREO Others<br />
• Contract for DoD<br />
commercial space<br />
access in development<br />
by STP<br />
46
STP Areas of Expertise:<br />
Rideshare<br />
Hosted Payloads Launch Rideshare Commercial<br />
Augmenting<br />
Mission<br />
Rideshare<br />
Prime Mission<br />
Partnership<br />
CMEWS on NASA STEREO<br />
Lower Cost<br />
FASTSat<br />
Maximizing<br />
Margin<br />
ESPA on STP-1<br />
Others<br />
• Enable rapid access to<br />
space through commercial<br />
means<br />
• Contract to be accessible to<br />
other gov agencies<br />
*Contract for Commercial <strong>Space</strong> Access<br />
in Development by STP<br />
47
Transition to<br />
Commercial<br />
Product<br />
MPACS<br />
•Design to space flt<br />
to commercial<br />
product<br />
•Abbreviated<br />
timeline<br />
•Continued<br />
manufacturing base<br />
Risk<br />
Reduction<br />
SAVE<br />
•Repackage<br />
complex system<br />
•Reduced SWAP<br />
•Lower integration<br />
cost<br />
Tech Demo<br />
SASSA<br />
•On-orbit proof of<br />
concept<br />
•Flexible on-orbit<br />
testing<br />
Tech Transition<br />
Operational<br />
Transition<br />
C/NOFS<br />
•On-orbit proof of<br />
concept<br />
•Significant valueadded<br />
to warfighter<br />
•Sensors being<br />
included in next-gen<br />
systems<br />
Planned<br />
Operational<br />
Use<br />
TacSat-3<br />
•Exp. direct to<br />
operations<br />
•Highly responsive<br />
•New capability<br />
direct to warfighter<br />
Risk Reduction and T 2 can be accomplished most effectively<br />
through either the SERB or STP partnership<br />
48
STPSat-3<br />
Flt Ready: FY12<br />
Projected Launch: FY13<br />
STP-2<br />
Possible Prime PL or<br />
Open ESPA Slots<br />
Partnership Opportunities<br />
ESPA SS<br />
1 ESPA Ring/yr<br />
• Starting in FY-13<br />
STPSat-4<br />
Future STP Satellite:<br />
• Possible bulk buy or<br />
rideshare<br />
Commercial<br />
Rideshare<br />
GEO<br />
Others<br />
BAA : Available to<br />
reimbursable customers<br />
Possible Rideshare or<br />
hosted PL<br />
49
CubeSats<br />
50
BAA<br />
51
Motivation<br />
• The number of SERB experiments is increasing every<br />
year<br />
• The STP budget is decreasing based on inflation<br />
adjustments<br />
• Technical demands of high ranked SERB experiments<br />
drive costs, limiting funds for lower ranked experiments<br />
• Elimination of the shuttle significantly impacts low cost<br />
flight opportunities<br />
• Commercial Rideshare appears to expand access to<br />
space with comparable costs<br />
STP needs additional cost effective opportunities for<br />
access to space<br />
52
DOD SERB<br />
.<br />
2010 SERB List<br />
73 Experiments<br />
.<br />
STP<br />
<strong>Space</strong>flight<br />
• Dedicated<br />
Missions<br />
• Shuttle/ISS<br />
• Auxiliaries<br />
Develop<br />
Commercial<br />
Capability<br />
Current<br />
Future<br />
Method<br />
Top Level Strategy<br />
Overarching (<strong>Program</strong> Top Level) Strategy<br />
2012 2014 2016<br />
<strong>Space</strong> Vehicle Payloads<br />
Hosted Payloads<br />
BAA: New Capability<br />
Development / Study<br />
Acq Strategy<br />
For Representative<br />
Set of Experiments<br />
Contracted Studies<br />
STP Payloads Commercially Hosted<br />
TBD: Sustainable Capability<br />
Acq Strategy for<br />
Long Term Commercial<br />
Hosting Arrangements<br />
Future Contracts<br />
53<br />
53
SERB Growth<br />
54
FY10 Dollars(In Millions)<br />
90<br />
80<br />
70<br />
60<br />
50<br />
40<br />
30<br />
20<br />
10<br />
0<br />
Experiment Growth over 11 years<br />
SERB Experiments Linear (SERB Experiments)<br />
FY90 FY91 FY92 FY93 FY94 FY95 FY96 FY97 FY98 FY99 FY00 FY01 FY02 FY03 FY04 FY05 FY06 FY07 FY08 FY09 FY10 FY11<br />
55
Infusion Pump<br />
A pocket-sized intravenous (IV) fluid pump used to<br />
infuse wounded personnel in forward areas without<br />
the need for a large elevated IV bag<br />
Life Support for Trauma Transport (LSTAT)<br />
A 21st century stretcher containing medical<br />
technologies of modern ICUs including remote<br />
patient monitoring and care devices<br />
Chitosan Bandages<br />
These bandages actively clot wounds without direct<br />
pressure to stem blood loss, the leading cause of<br />
battlefield casualties. On STS-118, Aug ‘07 CCM-A<br />
took the raw cytokines in Chitosan to test their<br />
unique antibacterial effects, expanding upon this<br />
fielded technology<br />
STP Warfighter Impact<br />
LSTAT<br />
(30 deployed)<br />
HEMCON bandages<br />
(1 ea. every service member<br />
In Iraq and Afghanistan)<br />
STP Technologies Impacting Tactical Operations Today<br />
Infusion<br />
Pump<br />
(10,000 in service)<br />
56
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