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On the Cusp: What’s Next
DARPA Perspective on Space
Ms. Pamela A. Melroy, Deputy Director, Tactical Technology Office
Briefing prepared for 53rd Robert H. Goddard Memorial Symposium
March 12, 2015
Approved for Public Release (DISTAR 24265), Distribution Unlimited.
The Defense Advanced Research Projects Agency (DARPA)
was established in 1958 to prevent strategic surprise
from negatively affecting U.S. national security and create
strategic surprise for U.S. adversaries by maintaining the
technological superiority of the U.S. military.
To fulfill its mission, the Agency relies on diverse
performers to apply multi-disciplinary approaches to both
advance knowledge through basic research and create
innovative technologies that address current practical
problems through applied research.
As the DoD’s primary innovation engine, DARPA
undertakes projects that are finite in duration but that
create lasting revolutionary change.
Mission
2Approved for Public Release (DISTAR 24265), Distribution Unlimited.
• Current launch has no surge capability and long call-up times
• 2+ years to get “into the queue”
• Maserati custom-built production line of a few vs.
Ford assembly line of thousands
• Fixed launch sites are vulnerable
Flexibility Has Not Been a Priority
© Reuters
© NOAA
3
© Maserati
© NASA
Approved for Public Release (DISTAR 24265), Distribution Unlimited.
Space Domain Awareness (SDA) Today
~16,000+ objects in 1014 km3 (240,000 oceans)
GEO
MEO
Can characterize †
NumberofObjects
LEO
Known
objects in
LEO orbit
≈ 12,020
Can’t detect & track Can detect & track †
Can
characterize †Can’t detect & track Can detect & track †
Can characterize †Can’t detect & track Can detect & track †
4
Size of Objects (RCS m2)
U.S. satellites
International satellites
U.S. debris
International debris
KEY
† Cannot detect, track and
characterize every object
simultaneously
Known
objects in
MEO orbit
≈ 1,890
SWISSCUBE
RCS: 0.041 m2
COSMOS 2080
RCS: 1.0 m2
NAVSTAR 64
RCS: 6.3 m2
ISS
RCS: 227.8 m2
Vanguard 1
RCS: 0.11 m2
Known
objects in
GEO orbit
≈ 1,840
*data as of 2015 Approved for Public Release (DISTAR 24265), Distribution Unlimited.
Launch:
• Flexible, affordable access
• Affordable, routine and reliable access to space
• Aircraft-like space access to lower cost and increase capabilities
• Small satellite access to GEO
Satellite:
• Changing the paradigm of satellite operations
• New satellite architectures for speed and robustness
• GEO space robotics to repair and assemble very large satellites that could not be
launched
Space Domain Awareness (SDA):
• Real-time space domain awareness
• Real-time detection and tracking versus catalog maintenance and days to weeks of
forensics
DARPA Vision for Robust Space
5Approved for Public Release (DISTAR 24265), Distribution Unlimited.
Flexible, Affordable Access to Space
6Approved for Public Release (DISTAR 24265), Distribution Unlimited.
Artist’s concept
Airborne Launch Assist Space Access (ALASA)
ALASA aims to:
• Leverage performance, flexibility and re-
usability of air launch, and streamlined design
and manufacturing
• Reduce infrastructure costs by using runways
vs. fixed sites, automating operations;
avoiding unnecessary services
• Launch 100-pound payloads for under $1M
per flight, including range costs
• Have the satellite on orbit 24 hours after the
request
• Escape the constraints of fixed direction and
location for space launch
• Exercise the concept frequently enough to
make operations increasingly efficient and
cost-effective
Goal: Provide more affordable, routine and reliable access to space for multiple missions
Todays capabilities: Vertical launch
Future capabilities: Horizontal launch
7Approved for Public Release (DISTAR 24265), Distribution Unlimited.
ALASA Design Emphasizes Features to Enable Lower
Unit Cost
• Two-stage liquid-fueled launch vehicle would use high
energy liquid monopropellant for simplified system
design and handling
• “Tractor” configuration would allow enhanced
performance
• Differential throttling and tangential canting would
eliminate gimbals and attitude jets
• Launching from unmodified F-15E aircraft would
leverage existing infrastructure for fast response and
low cost
• Commercial-grade avionics, advanced composite
structures, automated mission planning and flight
termination systems would reduce costs
Artist’s concept
Artist’s concept
Artist’s concept
Artist’s concept
8Approved for Public Release (DISTAR 24265), Distribution Unlimited.
• ALASA had a successful Phase I, which resulted in three viable system designs and three
enabling technologies that continued on into Phase II (engine test and critical design
review)
• Payload depends on delivered engine performance with new monopropellant, which will be
verified by testing beginning in February 2015
• DARPA has approved Phase III: 12 orbital test launched in 2015 and 2016; the smallsat
community is excited about having dedicated launch opportunities, and there has been no
difficulty finding useful payloads
Summary
Artist’s Concept
Artist’s Concept
9Approved for Public Release (DISTAR 24265), Distribution Unlimited.
XS-1 aims to:
• Break cycle of escalating space system
costs by:
• Enabling future space system
architectures
• Leveraging interests & capabilities of
commercial sector and space tourism
• Expand the reusable air-launched
concept with a hypersonic vehicle
capable of launching 3,000- to 5,000-
lbs payloads for $5M with low-cost
upper stage
• Mature and integrate technologies
supporting launch and hypersonic
vehicles
• Demonstrate mission assurance by
flying 10 times in 10 days
Experimental Spaceplane (XS-1)
Goal: Lower launch costs and increase space capabilities with aircraft-like space access
10
Artist’s Concept
Artist’s Concept
Artist’s Concept
Approved for Public Release (DISTAR 24265), Distribution Unlimited.
XS-1
Booster
Engine 2 Merlins
GLOW (K lbs) 223.9
MECO (K lbs) 47.4
Usable LOX/RP (K lbs) 176.5
Isp (vac) 310
Stage PMF 0.84
Upper Stage
GLOW (lbs) 15.0
Isp (vac) 336
Stage PMF 0.9
Payload (K lbs) 3.0 0 100 200 300 400 500 600
Altitude,Kft
Downrange, nmi
2-Stage Vehicle (GLOW-223.9K
lbs)
Booster (2-Merlins)
Propellant = 176.5K lbs
ISP (vac) = 310 sec
PMF = 0.84
Upper Stage (GLOW-15K lbs)
ISP (vac) = 336 sec
Staging:
Time = 169.9 sec
DR = 71.9 nmi
Altitude = 237,155 ft
Mach = 10.8
Payload = 3,025 lbm
100x100 nmi
28.5 deg Inclination
700
600
500
400
300
200
100
0
Notional X-Plane Upper Stage Trades
Expendable stage ~5%
of stack weight
Mach 10 staging with small upper stage (shown)
Alternative would be Mach 5 staging with larger upper stage
Artist’s Concept
11Approved for Public Release (DISTAR 24265), Distribution Unlimited.
XS-1 Summary
12
Artist’s concept
XS-1 aims to create a new paradigm for more routine,
responsive and affordable space operations
12
Artist’s concept
Artist’s concept
Approved for Public Release (DISTAR 24265), Distribution Unlimited.
XS-1 seeks to:
- Address growing launch costs in an era of
declining budgets
- Lower operating costs to enable new,
game-changing capabilities
- Leverage emerging suborbital launch
technology & entrepreneurs
- Demonstrate technology for transition to
government and commercial users
Payload Orbital Delivery (POD) System
• A standardized mechanism designed to safely carry
and release in GEO a wide variety of payloads aboard
commercial communications satellites
• Increase opportunities for small mass (~70-100 kg) to
many orbits (including GEO):
• High-tempo launches
• POD payload is agnostic to launch vehicle,
interfacing instead with the GEO host spacecraft
• Provide opportunities for rideshare and separation
from a host:
• Adjustable, precise and reliable payload ejection
• Low POD tumble rates for safe release
• Low dynamic disturbance to host
• Increase responsiveness:
• Efficient integration, testing and qualification,
and minimized need for re-verification, allowing
for late integration to the hosting satellite
• Flexibility in payload geometry and CG location
13
Artist’s concept
Approved for Public Release (DISTAR 24265), Distribution Unlimited.
Changing the Paradigm of Satellite Operations
14Approved for Public Release (DISTAR 24265), Distribution Unlimited.
Satlets
eXperiment for Cellular Integration
Technologies
(eXCITe)
Orbit: 450x720
98 deg
Date: 1QFY16
Life: 2-8 weeks
Launch: 1 of 5 payloads on a SHERPA
Objectives:
1. Demonstrate aggregation ability to withstand
launch environment, perform and maintain
thermal control, communicate with the ground,
reconstitute traditional spacecraft bus capability
2. Demonstrate aggregation ability to support a
simple and a complex payload
15
Artist’s concept
Artist’s concept
• A new low-cost, modular satellite
architecture that can scale almost infinitely
• Satlets are small modules that incorporate
multiple essential satellite functions and
share data, power and thermal
management capabilities
• Satlets physically aggregate in different
combinations that would provide
capabilities to accomplish diverse missions
Approved for Public Release (DISTAR 24265), Distribution Unlimited.
• Provide unparalleled
high-resolution images
on request of spacecraft
experiencing anomalies
• Inspections would be
enabled by a RMMV with
a sensor suite and
dexterous arms with
cameras
• Stand-off inspections
(50m-1km)
• Close inspections (5m-
50m)
• Docked inspections
Future Goal: GEO Robotic Servicing
• Cooperatively move
spacecraft in orbit,
recover spacecraft in off-
nominal orbits and extend
lifetimes through
propellant conservation
• N/S station keeping
recovery
• End-of-Life to GEO
graveyard
• Repositioning within the
GEO belt
• Assist spacecraft
experiencing
anomalies, helping to
ensure that missions can
be completed at
maximum performance
• Free stuck appendages
• Supplement attitude
control
• Perform docked
inspections
Artist’s
Concept
Artist’s
Concept
Artist’s
Concept
16Approved for Public Release (DISTAR 24265), Distribution Unlimited.
GEO servicing Could Build Confidence to
Transform the Entire Space ArchitectureSERVICING
First robotic
capability in GEO
Commercial
providers expand
coverage
NEWARCHITECTURES
LEO-to-GEO
space tug
• On-orbit replaceable units
• Modular spacecraft
Large apertures,
structures and bases
Automated,
scheduled
refueling
• Reduced
redundancy
• Lightly fueled
at launch
• Assembly
experiments
Technology development and investment
Space robotics = national-level growth potential
17Approved for Public Release (DISTAR 24265), Distribution Unlimited.
Real-Time Space Domain Awareness
18Approved for Public Release (DISTAR 24265), Distribution Unlimited.
OrbitOutlook
19
• Space Situational
Awareness (SSA)
currently uses
sophisticated and
exquisite certified
government sensors
• With this model,
greater coverage can
only come at a
significant cost Artist Concept
Government ground
based sensors
Joint Space
Operations Center
Government space
based sensors
Space object
Goal: Leverage hundreds of available, low-cost assets to increase coverage and
persistence of tracking space objects
Artist’s Concept
Approved for Public Release (DISTAR 24265), Distribution Unlimited.
OrbitOutlook
Government ground
based sensors
Commercial RF
tracking
University optical tracking
Joint Space
Operations Center
Data gathering
and analysis
International
partner data
Space object
Commercial
optical tracking
Artist’s Concept
Government space
based sensors
OrbitOutlook aims to:
• Integrate space
surveillance data from
non-traditional DoD
sources
• Commercial
• Academia
• International partners
• Establish processes to
verify information
assurance and data
quality
• Develop characterization
and Indications and
Warning (I&W)
techniques
20
Goal: Leverage hundreds of available, low-cost assets to increase coverage and
persistence of tracking space objects
Approved for Public Release (DISTAR 24265), Distribution Unlimited.
Hallmark: Real-Time Space Domain Awareness
21
Goals:
• Perform real-time information fusion,
including course of action (COA)
generation and execution support
• Ingest source-agnostic information
• Use automation algorithms as decision
aids to meet specific timelines
• Develop 3D visualization containing
intuitive commander operating picture
Provide U.S. senior leadership the tools needed for real-time understanding and evaluation
of the space environment
Artist’s Concept
Approved for Public Release (DISTAR 24265), Distribution Unlimited.
Creating the Future
Routine access to spaceGEO robotic servicing
Tactical space traffic control
DARPA space programs could help enable
breakthrough future technologies in many
areas, including:
• Tactical space traffic control
• GEO robotic servicing
• Routine access to space
DARPA seeks to fuel and leverage commercial
capabilities, and partner with other agencies to
augment national and economic security
22
Artist’s concept
Artist’s concept
Approved for Public Release (DISTAR 24265), Distribution Unlimited.
Artist’s concept
www.darpa.mil
23Approved for Public Release (DISTAR 24265), Distribution Unlimited.

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Goddard 2015: Pamela Melroy, DARPA

  • 1. On the Cusp: What’s Next DARPA Perspective on Space Ms. Pamela A. Melroy, Deputy Director, Tactical Technology Office Briefing prepared for 53rd Robert H. Goddard Memorial Symposium March 12, 2015 Approved for Public Release (DISTAR 24265), Distribution Unlimited.
  • 2. The Defense Advanced Research Projects Agency (DARPA) was established in 1958 to prevent strategic surprise from negatively affecting U.S. national security and create strategic surprise for U.S. adversaries by maintaining the technological superiority of the U.S. military. To fulfill its mission, the Agency relies on diverse performers to apply multi-disciplinary approaches to both advance knowledge through basic research and create innovative technologies that address current practical problems through applied research. As the DoD’s primary innovation engine, DARPA undertakes projects that are finite in duration but that create lasting revolutionary change. Mission 2Approved for Public Release (DISTAR 24265), Distribution Unlimited.
  • 3. • Current launch has no surge capability and long call-up times • 2+ years to get “into the queue” • Maserati custom-built production line of a few vs. Ford assembly line of thousands • Fixed launch sites are vulnerable Flexibility Has Not Been a Priority © Reuters © NOAA 3 © Maserati © NASA Approved for Public Release (DISTAR 24265), Distribution Unlimited.
  • 4. Space Domain Awareness (SDA) Today ~16,000+ objects in 1014 km3 (240,000 oceans) GEO MEO Can characterize † NumberofObjects LEO Known objects in LEO orbit ≈ 12,020 Can’t detect & track Can detect & track † Can characterize †Can’t detect & track Can detect & track † Can characterize †Can’t detect & track Can detect & track † 4 Size of Objects (RCS m2) U.S. satellites International satellites U.S. debris International debris KEY † Cannot detect, track and characterize every object simultaneously Known objects in MEO orbit ≈ 1,890 SWISSCUBE RCS: 0.041 m2 COSMOS 2080 RCS: 1.0 m2 NAVSTAR 64 RCS: 6.3 m2 ISS RCS: 227.8 m2 Vanguard 1 RCS: 0.11 m2 Known objects in GEO orbit ≈ 1,840 *data as of 2015 Approved for Public Release (DISTAR 24265), Distribution Unlimited.
  • 5. Launch: • Flexible, affordable access • Affordable, routine and reliable access to space • Aircraft-like space access to lower cost and increase capabilities • Small satellite access to GEO Satellite: • Changing the paradigm of satellite operations • New satellite architectures for speed and robustness • GEO space robotics to repair and assemble very large satellites that could not be launched Space Domain Awareness (SDA): • Real-time space domain awareness • Real-time detection and tracking versus catalog maintenance and days to weeks of forensics DARPA Vision for Robust Space 5Approved for Public Release (DISTAR 24265), Distribution Unlimited.
  • 6. Flexible, Affordable Access to Space 6Approved for Public Release (DISTAR 24265), Distribution Unlimited.
  • 7. Artist’s concept Airborne Launch Assist Space Access (ALASA) ALASA aims to: • Leverage performance, flexibility and re- usability of air launch, and streamlined design and manufacturing • Reduce infrastructure costs by using runways vs. fixed sites, automating operations; avoiding unnecessary services • Launch 100-pound payloads for under $1M per flight, including range costs • Have the satellite on orbit 24 hours after the request • Escape the constraints of fixed direction and location for space launch • Exercise the concept frequently enough to make operations increasingly efficient and cost-effective Goal: Provide more affordable, routine and reliable access to space for multiple missions Todays capabilities: Vertical launch Future capabilities: Horizontal launch 7Approved for Public Release (DISTAR 24265), Distribution Unlimited.
  • 8. ALASA Design Emphasizes Features to Enable Lower Unit Cost • Two-stage liquid-fueled launch vehicle would use high energy liquid monopropellant for simplified system design and handling • “Tractor” configuration would allow enhanced performance • Differential throttling and tangential canting would eliminate gimbals and attitude jets • Launching from unmodified F-15E aircraft would leverage existing infrastructure for fast response and low cost • Commercial-grade avionics, advanced composite structures, automated mission planning and flight termination systems would reduce costs Artist’s concept Artist’s concept Artist’s concept Artist’s concept 8Approved for Public Release (DISTAR 24265), Distribution Unlimited.
  • 9. • ALASA had a successful Phase I, which resulted in three viable system designs and three enabling technologies that continued on into Phase II (engine test and critical design review) • Payload depends on delivered engine performance with new monopropellant, which will be verified by testing beginning in February 2015 • DARPA has approved Phase III: 12 orbital test launched in 2015 and 2016; the smallsat community is excited about having dedicated launch opportunities, and there has been no difficulty finding useful payloads Summary Artist’s Concept Artist’s Concept 9Approved for Public Release (DISTAR 24265), Distribution Unlimited.
  • 10. XS-1 aims to: • Break cycle of escalating space system costs by: • Enabling future space system architectures • Leveraging interests & capabilities of commercial sector and space tourism • Expand the reusable air-launched concept with a hypersonic vehicle capable of launching 3,000- to 5,000- lbs payloads for $5M with low-cost upper stage • Mature and integrate technologies supporting launch and hypersonic vehicles • Demonstrate mission assurance by flying 10 times in 10 days Experimental Spaceplane (XS-1) Goal: Lower launch costs and increase space capabilities with aircraft-like space access 10 Artist’s Concept Artist’s Concept Artist’s Concept Approved for Public Release (DISTAR 24265), Distribution Unlimited.
  • 11. XS-1 Booster Engine 2 Merlins GLOW (K lbs) 223.9 MECO (K lbs) 47.4 Usable LOX/RP (K lbs) 176.5 Isp (vac) 310 Stage PMF 0.84 Upper Stage GLOW (lbs) 15.0 Isp (vac) 336 Stage PMF 0.9 Payload (K lbs) 3.0 0 100 200 300 400 500 600 Altitude,Kft Downrange, nmi 2-Stage Vehicle (GLOW-223.9K lbs) Booster (2-Merlins) Propellant = 176.5K lbs ISP (vac) = 310 sec PMF = 0.84 Upper Stage (GLOW-15K lbs) ISP (vac) = 336 sec Staging: Time = 169.9 sec DR = 71.9 nmi Altitude = 237,155 ft Mach = 10.8 Payload = 3,025 lbm 100x100 nmi 28.5 deg Inclination 700 600 500 400 300 200 100 0 Notional X-Plane Upper Stage Trades Expendable stage ~5% of stack weight Mach 10 staging with small upper stage (shown) Alternative would be Mach 5 staging with larger upper stage Artist’s Concept 11Approved for Public Release (DISTAR 24265), Distribution Unlimited.
  • 12. XS-1 Summary 12 Artist’s concept XS-1 aims to create a new paradigm for more routine, responsive and affordable space operations 12 Artist’s concept Artist’s concept Approved for Public Release (DISTAR 24265), Distribution Unlimited. XS-1 seeks to: - Address growing launch costs in an era of declining budgets - Lower operating costs to enable new, game-changing capabilities - Leverage emerging suborbital launch technology & entrepreneurs - Demonstrate technology for transition to government and commercial users
  • 13. Payload Orbital Delivery (POD) System • A standardized mechanism designed to safely carry and release in GEO a wide variety of payloads aboard commercial communications satellites • Increase opportunities for small mass (~70-100 kg) to many orbits (including GEO): • High-tempo launches • POD payload is agnostic to launch vehicle, interfacing instead with the GEO host spacecraft • Provide opportunities for rideshare and separation from a host: • Adjustable, precise and reliable payload ejection • Low POD tumble rates for safe release • Low dynamic disturbance to host • Increase responsiveness: • Efficient integration, testing and qualification, and minimized need for re-verification, allowing for late integration to the hosting satellite • Flexibility in payload geometry and CG location 13 Artist’s concept Approved for Public Release (DISTAR 24265), Distribution Unlimited.
  • 14. Changing the Paradigm of Satellite Operations 14Approved for Public Release (DISTAR 24265), Distribution Unlimited.
  • 15. Satlets eXperiment for Cellular Integration Technologies (eXCITe) Orbit: 450x720 98 deg Date: 1QFY16 Life: 2-8 weeks Launch: 1 of 5 payloads on a SHERPA Objectives: 1. Demonstrate aggregation ability to withstand launch environment, perform and maintain thermal control, communicate with the ground, reconstitute traditional spacecraft bus capability 2. Demonstrate aggregation ability to support a simple and a complex payload 15 Artist’s concept Artist’s concept • A new low-cost, modular satellite architecture that can scale almost infinitely • Satlets are small modules that incorporate multiple essential satellite functions and share data, power and thermal management capabilities • Satlets physically aggregate in different combinations that would provide capabilities to accomplish diverse missions Approved for Public Release (DISTAR 24265), Distribution Unlimited.
  • 16. • Provide unparalleled high-resolution images on request of spacecraft experiencing anomalies • Inspections would be enabled by a RMMV with a sensor suite and dexterous arms with cameras • Stand-off inspections (50m-1km) • Close inspections (5m- 50m) • Docked inspections Future Goal: GEO Robotic Servicing • Cooperatively move spacecraft in orbit, recover spacecraft in off- nominal orbits and extend lifetimes through propellant conservation • N/S station keeping recovery • End-of-Life to GEO graveyard • Repositioning within the GEO belt • Assist spacecraft experiencing anomalies, helping to ensure that missions can be completed at maximum performance • Free stuck appendages • Supplement attitude control • Perform docked inspections Artist’s Concept Artist’s Concept Artist’s Concept 16Approved for Public Release (DISTAR 24265), Distribution Unlimited.
  • 17. GEO servicing Could Build Confidence to Transform the Entire Space ArchitectureSERVICING First robotic capability in GEO Commercial providers expand coverage NEWARCHITECTURES LEO-to-GEO space tug • On-orbit replaceable units • Modular spacecraft Large apertures, structures and bases Automated, scheduled refueling • Reduced redundancy • Lightly fueled at launch • Assembly experiments Technology development and investment Space robotics = national-level growth potential 17Approved for Public Release (DISTAR 24265), Distribution Unlimited.
  • 18. Real-Time Space Domain Awareness 18Approved for Public Release (DISTAR 24265), Distribution Unlimited.
  • 19. OrbitOutlook 19 • Space Situational Awareness (SSA) currently uses sophisticated and exquisite certified government sensors • With this model, greater coverage can only come at a significant cost Artist Concept Government ground based sensors Joint Space Operations Center Government space based sensors Space object Goal: Leverage hundreds of available, low-cost assets to increase coverage and persistence of tracking space objects Artist’s Concept Approved for Public Release (DISTAR 24265), Distribution Unlimited.
  • 20. OrbitOutlook Government ground based sensors Commercial RF tracking University optical tracking Joint Space Operations Center Data gathering and analysis International partner data Space object Commercial optical tracking Artist’s Concept Government space based sensors OrbitOutlook aims to: • Integrate space surveillance data from non-traditional DoD sources • Commercial • Academia • International partners • Establish processes to verify information assurance and data quality • Develop characterization and Indications and Warning (I&W) techniques 20 Goal: Leverage hundreds of available, low-cost assets to increase coverage and persistence of tracking space objects Approved for Public Release (DISTAR 24265), Distribution Unlimited.
  • 21. Hallmark: Real-Time Space Domain Awareness 21 Goals: • Perform real-time information fusion, including course of action (COA) generation and execution support • Ingest source-agnostic information • Use automation algorithms as decision aids to meet specific timelines • Develop 3D visualization containing intuitive commander operating picture Provide U.S. senior leadership the tools needed for real-time understanding and evaluation of the space environment Artist’s Concept Approved for Public Release (DISTAR 24265), Distribution Unlimited.
  • 22. Creating the Future Routine access to spaceGEO robotic servicing Tactical space traffic control DARPA space programs could help enable breakthrough future technologies in many areas, including: • Tactical space traffic control • GEO robotic servicing • Routine access to space DARPA seeks to fuel and leverage commercial capabilities, and partner with other agencies to augment national and economic security 22 Artist’s concept Artist’s concept Approved for Public Release (DISTAR 24265), Distribution Unlimited. Artist’s concept
  • 23. www.darpa.mil 23Approved for Public Release (DISTAR 24265), Distribution Unlimited.

Hinweis der Redaktion

  1. DISTAR Case 20999
  2. DISTAR Case 24081 Maserati image: www.maserati.com Reuters image: http://www.reuters.com/article/2012/05/14/us-ford-china-idUSBRE84D03C20120514 Hurricane image: NOAA US Government image http://www1.ncdc.noaa.gov/pub/data/images/hurricane-fran-nasa1.gif Radar image: SMDC US Government Image http://www.smdc.army.mil/SMDCPhoto_Gallery/Sensors/Radar.jpg Launchpad image: NASA US Government Image http://dayton.hq.nasa.gov/IMAGES/LARGE/GPN-2000-000869.jpg
  3. DISTAR Case 24158 Rough cut LEO – apogee below 2,000 km GEO – apogee 35,786 +/- 2,000 km MEO – apogee between LEO and GEO
  4. DISTAR Case 24081
  5. DISTAR Case 24081
  6. DISTAR Case 24081
  7. DISTAR Case 24081
  8. DISTAR Case 24081
  9. DISTAR Case 24081
  10. DISTAR Case 23655
  11. The image on the bottom left of slide is the LADEE spacecraft bus while it was being assembled. LADEE had a modular design, so it is just an example of the fact that modular spacecraft are feasible. (LADEE was not designed to have modules replaced or assembled on orbit, however; its modularity was just for ground assembly.) (LADEE was a NASA spacecraft that recently orbited the Moon.) “First Robotic” and “Commercial Providers” images from NRL All other images from NASA
  12. DISTAR Case 24158
  13. DISTAR Case 24158
  14. DISTAR Case 24158
  15. DISTAR Case 24158