HAWAII AEROSPACE SUMMIT Steve Skladanek Director of Marketing, Lockheed Martin Commercial Launch Services THEME : Commercial Space Lift from Hawaii: - Advantages and Challenges • Orbital Mechanics 101 • Two for One in the Safety Department • Infrastructure • The Business of Space Lift [ 1 ]
2 topic panel 1
Jan 16, 2015
Commercial Space Lift from Hawaii: - Advantages and Challenges presented by Steve Skladanek , Director of Marketing, Lockheed Martin Commercial Launch Services
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HAWAII
AEROSPACE
SUMMIT
Steve SkladanekDirector of Marketing, Lockheed Martin Commercial Launch Services
THEME: Commercial Space Lift from Hawaii:- Advantages and Challenges
•Orbital Mechanics 101
•Two for One in the Safety Department
•Infrastructure
•The Business of Space Lift
[ 1 ]
Hawai`i Space Flight LaboratoryUniversity of Hawai`i at Mānoa
2013 Hawaii Aerospace Summit
Topic Panel 1: Space Transportation
Presenter:
Dr. Luke Flynn
Director, Hawaii Space Flight Laboratory
Main Points: HSFL executes State-wide small satellite launch program ORS-4 Mission slated for 2014 orbital launch from PMRF
UH Role in Future Hawaii Aerospace Industry
3
Distribution A: Unclassified - Cleared for Public Release
UH Support Elements for Orbital Satellites
S/C SystemsAvionicsPowerTelecomThermalS/WH/W
•UH/HSFL maintains UHF/VHF receiving stations with Kauai CC and Honolulu CC staff.•Ground station provides command and control broadcast as well as data downlink capabilities.•Mission Ops Center on POST 5th floor under development with UH support.
Ground Station & Mission OperationsLaunch Vehicle and Launch Support• Pacific Missile Range Facility (PMRF)•Local launch facility and mission support •Modify existing PMRF launch pad for rail-fitted and modified VAFB Scout launcher.
• Kauai Test Facility (KTF)/ Sandia National Lab•Experience with solid rockets and missile design. Use Super-Strypi launch vehicle.•Can send ~270 kg (594 pounds) to low-Earth orbit (400 km).•Heritage working with PMRF as vehicle integrator and launch agent.
Integration and Test• Clean rooms in UH/POST will be used to assemble satellites.
– Systems integration– Thermo-vac testing– Vibration/shock testing– Payload spin balancing
Spacecraft• Partner with NASA Centers and others to advance small spacecraft design.•Design, build, launch, and operate 1-100 kg small satellite for science and education tasks.•Support technology validation missions as well as other University missions.
Instruments•The HSFL can call on a diverse group of instrument-developing faculty from HIGP and SOEST.
•A number of businesses in Hawaii also develop a wide array of instrumentation. The HSFL will partner with these organizations to provide technology demonstration opportunities.
•NASA Centers (Ames and JPL) are interested in joint technology missions.
4
ORS-4 Mission: Fully Funded for Summer 2014 launch The Operationally Responsive Space Office with support
from the Sandia National Laboratories, University of Hawaii and other partners is developing a orbital small launch vehicle. Goal is to deliver 300kg to Low Earth Orbit (LEO). Develop and test fly three new solid rocket motors from
Aerojet-Rocketdyne. Future mission cost is $15-18M/launch compared to +
$30M for other US alternatives. UH/HSFL’s HiakaSat will fly as the primary payload on the
Integrated Payload Stack UH hyperspectral imager flies on HiakaSat.
Partnerships Developed Space Act Agreement with NASA Ames:
Development of HiakaSat Strategic Alliance Agreement with Aerojet-
Rocketdyne: Solid rocket motors Pacific Missile Range Facility: Support for all HSFL
activities Sandia National Laboratory: Rocket development Alaska Aerospace Corporation: Future launch
opportunities for small sats *Northrop-Grumman: Space technology test-bed on
HiakaSat * USPACOM: Discussions and guidance regarding
Department of Defense future needs.
Super-Strypi
Distribution A: Unclassified - Cleared for Public Release 5
AJR motor test -2012
HiakaSat
SUCHI
Engaging the UH System: Workforce Development
Distributed campus approach to workforce development. CC’s provide technical Associate Degrees 4-yr provide depth in Bachelor’s Degrees
Present Status and Future Plan: Kauai: Small satellite communications and electronics fabrication,
CubeSat development Maui: Space debris surveillance and removal – NASA JSC interest Hawaii: Software development for small satellites, test bed for
HSFL lunar rovers Oahu: CubeSat development at HCC, WCC, LCC, KCC (won
national award for CanSat); satellite data reception at UH-Manoa, HCC; mission control at UH-Manoa, small sat development at UH-Manoa; launch vehicle integration and safety training at WCC and UH-Manoa.
6
Status
OBCS
EPS
ADCS
Telecom
TCS
Payloads
FSW
GS
x 10-1
x 100
UTC MOC LocalT MET
Mode
Angle Rate
PitchRoll
Yaw
Units
Slew RateFlight Path
Spin RateSS 1SS 2SS 3
Orbit2012-01-23 19:43:07 08:43:07 14:43:07 1234:09:32:27 17126Umbra
KCC
CRATEXOrbital Events Spacecraft EventsUTC
19:40:00
19:45:00
19:50:00
19:55:00
20:00:00
20:05:00
20:10:00
20:15:00
20:20:00
19:35:00
19:30:00
19:25:00
19:20:00
19:15:00
19:10:00
NPole
N60D
N30D
DNode
S30D
S60D
N60A
N30A
ANode
OutUm [+0:05:17]
[-0:02:10]
[-0:14:46]
KCC AOS
KCC LOS Reset Bar
Zoom In
Zoom Out
CRATEX XPNDR ON
UPLOAD F#17126-B
[+0:09:12]
[-0:10:48]CRATEX XPNDR OFF
[-0:02:58]IMAGER-N SEQ 17126-A [-0:05:32]
R/T
SimulatedS/C Mode
2012/01/2319:43:07
Latitude
Longitude
Altitude
Sun Beta Angle
Time to Sunlight
View Options
EPS OBCS
Telecom
PayloadsBus VoltageBus Current
Power
Load
Battery Levels
A BCharging
Images
SSDR
Free
1
2 3 4
5
678
T
%
Transponder
Signal Lock
CRATEX Transponder 1CRATEX Transponder 2
CERTO Status
GPS Status
GPS Lock
Imager-N Status
Imager-Z Status
>
Orbit
100%75%50%25%
MB
ADCS
0.5
0
1.0
-1.0
0
-0.5
Reset
Reset
Beacon
Carrier THI Status
Time to Eclipse
Time to Sunlight
Status
OBCS
EPS
ADCS
Telecom
TCS
Payloads
FSW
GS
x 100
x 100
Status
OBCS
EPS
ADCS
Telecom
TCS
Payloads
FSW
GS
Status
OBCS
EPS
ADCS
Telecom
TCS
Payloads
FSW
GS
OBCS
EPS
ADCS
Telecom
TCS
Payloads
FSW
GS
x 10-1
x 100
UTC MOC LocalT MET
Mode
Angle Rate
PitchRoll
Yaw
UnitsUnits
Slew RateFlight Path
Spin RateSS 1SS 2SS 3
Orbit2012-01-23 19:43:07 08:43:0708:43:07 14:43:0714:43:07 1234:09:32:271234:09:32:27 17126Umbra
KCC
CRATEXOrbital Events Spacecraft EventsUTC
19:40:00
19:45:00
19:50:00
19:55:00
20:00:00
20:05:00
20:10:00
20:15:00
20:20:00
19:35:00
19:30:00
19:25:00
19:20:00
19:15:00
19:10:00
NPole
N60D
N30D
DNode
S30D
S60D
N60A
N30A
ANode
OutUm [+0:05:17]
[-0:02:10]
[-0:14:46]
KCC AOS
KCC LOS Reset Bar
Zoom In
Zoom Out
CRATEX XPNDR ON
UPLOAD F#17126-B
[+0:09:12]
[-0:10:48]CRATEX XPNDR OFF
[-0:02:58]IMAGER-N SEQ 17126-A [-0:05:32]
R/T
SimulatedS/C Mode
2012/01/2319:43:07
Latitude
Longitude
Altitude
Sun Beta Angle
Time to Sunlight
View Options
EPS OBCS
Telecom
PayloadsBus VoltageBus Current
Power
Load
Battery Levels
A BCharging
Images
SSDR
Free
1
2 3 4
5
678
T
%
Transponder
Signal Lock
CRATEX Transponder 1CRATEX Transponder 2
CERTO Status
GPS Status
GPS Lock
Imager-N Status
Imager-Z Status
>
Orbit
100%75%50%25%
MB
ADCS
0.5
0
1.0
-1.0
0
1.0
-1.0
0
-0.5
ResetReset
ResetReset
Beacon
Carrier THI Status
Time to Eclipse
Time to Sunlight
Status
OBCS
EPS
ADCS
Telecom
TCS
Payloads
FSW
GS
Status
OBCS
EPS
ADCS
Telecom
TCS
Payloads
FSW
GS
OBCS
EPS
ADCS
Telecom
TCS
Payloads
FSW
GS
x 100
x 100
COSMOS: Mission Control
CubeSats
Distribution A: Unclassified - Cleared for Public Release
HAWAII
AEROSPACE
SUMMIT
Brian Gulliver, PESpaceport Planning Lead, RS&H
THEME: Planning and Development of Hawaii’s Commercial Spaceport
• Site Selection and Evaluation
• Business Case Study
• Preliminary Environmental Analyses
• Environmental Assessment
[ 3 ]
HAWAII
AEROSPACE
SUMMIT
Brian Gulliver, PESpaceport Planning Lead, RS&H
[ 3 ]
Brian Gulliver, PESpaceport Planning Lead, RS&H
[ 3 ]
Proposed RLV Operating Area
HAWAII
AEROSPACE
SUMMIT
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