Agenda
Click here
for a full list of RASTE 2008 topic descriptions.
2008 Responsive Access to Space
Technology Exchange (RASTE)
|
Monday,
19 May 2008
|
| 1000-1700 |
Registration |
| 1000-1600 |
Exhibit and Poster Setup |
| 1230 -1330 |
FAST Overview, Mr. Jeff Zweber
and Maj Nidal Jodeh, AFRL/RB |
| 1330 |
Bus Pickup for Tours |
| 1400 - 1600 |
Wind Tunnel Facilities Tour
Click here for informative pdf
or Structural Test Facilities Tour
Click here for informative pdf |
| 1645 |
Tour Bus returns to Crowne
Plaza |
Tuesday, 20 May 2008
|
| 0700-0800 |
Continental Breakfast |
| 0700 - 1730 |
Registration |
| 0800-0805 |
Administrative Remarks, AFRL |
| 0805-0835 |
Science and Technology for Future
Launch, Dr. Michael A. Kuliasha is Chief Technologist, Air Force
Research Laboratory |
| 0835-0905 |
AFSPC Responsive Launch
Requirements, Lt Col Michael Bodtke, AFSPC/A5V |
| 0905-0935 |
SMC Space Lift Development Plan,
Col Kenneth Allison, SMC/XR |
| 0935-1005 |
ORS Future View of Responsive
Launch, Dr. Merri Sanchez, AFSPC SDTW/ORS |
| 1005-1020 |
BREAK |
| 1020-1035 |
Blackswift – Hypersonic X-Plane
Overview, Dr. Keith Numbers, AFRL/RBZ |
| 1035-1105 |
ORS-Lift, an Overview, Mr. Bruce
Thieman, AFRL/RBOT |
| 1105-1130 |
The NASA Technology Development
Portfolio for Space Vehicle Systems, Dr. Minoo Dastoor, NASA HQ |
| 1130-1200 |
SpaceShip Two/WhiteKnight Two, Mr.
George Whitesides, Virgin Galactic |
| 1200-1300 |
Lunch |
| 1230-1700 |
Private Industry Meetings (By
appointment.) |
| 1300-1620 |
Responsive Launch Vehicle
Materials and Material Testing & Processing Technologies
|
| 1300-1310 |
Opening Remarks |
| 1310-1335 |
Ceramic Acreage Thermal Protection
for Operationally Responsive Space Access, Mr. Tom Pinney,
Boeing/Phantom Works |
| 1335-1400 |
C-C Hot Structure for Rigid
Aeroshell, Dr. Suraj Rawal, Lockheed Martin Space Systems, Co. |
| 1400-1425 |
Hertzian Fracture, Kinetic Friction
and the Mechanical Impact LOX Compatibility Testing of Polymers
and Polymer Matrix Composites, Mr. Roger Gerzeski, AFRL/RXBC |
| 1425-1450 |
Metallic Thin Foil Test System
Development, Mr. Ryan Morrissey, AFRL/RXLM |
| 1450-1505 |
Break |
| 1505-1530 |
Arc-Heater Test Simulation of a
Carbon-Carbon Aeroshell Flying a Prompt Global Strike
Trajectory, Mr. Henry Moody, Thermal Technologies |
|
1530-1555 |
Technology Needs of Emerging Space
Companies: Thermal Protection Systems, Dr. Dan Rasky, NASA ARC |
| 1555-1620 |
NASA Development of Ceramic Matrix
Composites, Dr. Anthony Calomino, NASA LaRC |
| 1630-1730 |
Poster Session |
Poster
Presentations
|
| In Defense of Reusable Launch Vehicle Horizontal
Take-Off (RLV-HTO), Mr. Wes Kelley, Triton Systems, LLC |
| Pressure-fed, Two-Stage Expendable System for a
Reusable Booster, Dr. Robert Conger, Microcosm, Inc. |
| Simulation, Training, and Analysis For Fixed
Sites (STAFFS) Model, His name is Mr. Paul Kirk, GDIT - AFRL/RHPC/ |
| Reusable Launch Vehicle
Regeneration Modeling, Dr. Alan Johnson, AFIT/ENS |
Wednesday, 21
May 2008
|
| 0700-0800 |
Continental Breakfast |
| 0700 – 1700 |
Registration |
| 0900-1145 |
Private Industry Meetings (By
appointment.) |
| 0800-1200 |
Responsive Launch Vehicle Materials and
Material Testing & Processing Technologies (continued) |
Integrated System Health Management,
Guidance, and Control |
| 0800-0810 |
Opening Remarks |
Opening Remarks |
| 0810-0835 |
Design of Load-Bearing Integrated Acreage
Thermal Protection Systems, Ms. Kerry Dunfey, Materials Research
& Design, Inc. |
Integrated Adaptive Guidance and Control
Results from X-37 Hardware-in-the-loop Ground Experiment, Mr.
Paul Kubiatko, Boeing |
| 0835-0900 |
Passive Leading Edge Incorporating Carbon
Foam, Mr. Jim Ledesma, Boeing/Phantom Works |
Barron Associates's Reusable Launch Vehicle
Programs Overview, Dr. John Schierman, Barron Associates, Inc. |
| 0900-0925 |
The Development of Fabrication Methods for
2D Carbon-Carbon Heat Shield and Aeroshell Materials for
Advanced Re-entry Applications, Dr. John Shigley, ATK Launch
Systems |
Rocket Engine Health Management for
Responsive Access to Space, Mr. Paul Phillipsen, WASK
Engineering, Inc. |
| 0925-0950 |
Design of Weight Competitive Carbon-Carbon
Acreage Thermal Protection System Panels, Dr. Brian Sullivan,
Materials Research & Design, Inc. |
Cryo-TrackerŪ Mass Gauging System for
Launch Vehicle Propellant Monitoring and Management, Mr. Mark
Haberbusch, Sierra Lobo, Inc. |
| 0950-1005 |
Break |
Break |
| 1005-1030 |
Large Scale Manufacturing and Certification
of Carbon-Carbon Composites, Mr. Raj Narayanan, Carbon-Carbon
Advanced Technologies, Inc. |
TBD |
| 1030-1055 |
Thin Walled, All-Composite Cryogenic Tanks
for Launch Vehicle Applications, Dr. Robert Conger, Microcosm,
Inc. |
TPS Health Monitoring for Responsive Space
Access, Dr. Jerry Huang, Boeing/Phantom Works |
| 1055-1120 |
Advanced Design of Integrated Warm
Structures for a Composite RLV Airframe, Mr. Cliff Fukuda,
Northrop Grumman Integrated Systems |
Integrated Impact Detection System for Thermal Protection
System, Mr. Lien Ouyang, Acellent Technologies |
| 1120-1145 |
Development of High Temperature Heat Pipes
for Responsive Space Vehicles, Dr. Suraj Rawal, Lockheed Martin
Space Systems
|
Sensor Selection and Data Validation for
Reliable Integrated System Health Management, Mr. Sanjay Garg,
NASA GRC |
| 1145-1210 |
|
FAST IVHM, Mr. J.B. Schroeder, AFRL/RBCC |
| 1210-1330 |
Lunch |
| 1300-1700 |
Private Industry
Meetings (Two rooms, 20 – 30 minute increments) |
| 1330-1715 |
Responsive Launch
Vehicle Propulsion Technologies |
| 1330-1340 |
Opening Remarks |
| 1340-1405 |
ORBITEC Rocket
Propulsion Developments, Mr. Ron Teeter, Orbitec |
| 1405-1430 |
Integrated Powerhead
Demo - Highly Reusable LOX/LH2 Technologies,
Mr. Stephen
Hanna, AFRL/RZSE |
| 1430-1455 |
Solid Propulsion for
Small Launch Vehicles, Mr. John Remen, AFRL/RZS |
| 1455-1520 |
Improved SLV Technology
Maturation and Methodology, Mr. Nils Sedano, AFRL/RZSE |
| 1520-1535 |
Break |
| 1535-1600 |
XCOR Aerospace's
Progress in Pump-Fed Rocket Propulsion, Mr. Mike Valant, XCOR
Aerospace |
| 1600-1625 |
LO2/LCH4 14 klbf Rocket
Engine Development, Mr. Paul Phillipsen, WASK Engineering |
| 1625-1650 |
Lox-Methane Rocket
Engine Development and Testing Activities at ATK, Mr. Richard
Stone, ATK GASL Div. |
| 1650-1715 |
Modeling, Simulation &
Analysis Tools for Liquid and Solid Propulsion,
AFRL/RZS (Jackson & Tull) |
| 1715-1900 |
Exhibit and Poster
Paper Reception |
Thursday, 22 May
2008
|
| 0700-0800 |
Continental Breakfast |
| 0700 – 1530 |
Registration |
| 0900-1145 |
Private Industry Meetings (By
appointment.) |
| 0800-1200 |
Responsive Launch Vehicle
Integration Technologies |
| 0800-0810 |
Opening Remarks |
| 0810-0835 |
Technology Uncertainty Impact on
Fully Reusable Access-to-Space Options, Dr. Ajay Kothari, Astrox
Corporation |
| 0835-0900 |
Benchmarking CFD-based Aerodynamic
and Aerothermal Predictions for Reusable Launch Vehicles (RLVs)
in Hypersonic Flight, Mr. Kurt Acheson, Andrews Space |
| 0900-0925 |
Modeling and Simulation of Air and
Space Vehicles for USAF and NASA Applications, Mr. Adel Chemaly,
TechnoSoft, Inc. |
| 0925-0950 |
Innovative Concept Development of
Reusable Launch Vehicles (RLVs) Using Combined-Cycle Propulsion
for Military Applications, Dr. John Bradford, SpaceWorks
Engineering, Inc. |
| 0950-1005 |
Break |
| 1005-1030 |
AFRL Rocket Boost Back Systems
Analysis, Mr. Greg Moster, AFRL/RBS |
| 1030-1055 |
Aeroelastic Assessment, Mr. Scott
Zink, Lockheed Martin |
| 1055-1120 |
Wind Tunnel Testing for RLV
Configurations, Mr. Dan Tejtel, AFRL/RBAA |
| 1120-1145 |
Propulsion Integration for RLVs,
Mr. Nils Sedano, AFRL/RZS |
| 1145-1315 |
Lunch |
| 1245-1630 |
Private Industry Meetings (By
appointment.) |
| 1315-1635 |
Responsive Launch Vehicle
Systems Integrators |
| 1315-1325 |
Opening Remarks |
| 1325-1350 |
Overview of the NASA Aeronautics
Hypersonics Project, Dr. James Pittman, NASA LaRC |
| 1350-1415 |
Responsiveness as a Systems-level
Technology: The Lynx Mark II Nanosat Launch Capability,
Mr. James Muncy, XCOR Aerospace |
| 1415-1440 |
Inverted Reentry/Standard Reentry,
Mr. Tom Smith, Boeing |
| 1440-1505 |
FAST Configuration Development, Mr.
Jon Carpenter, Northrop Grumman |
| 1505-1520 |
Break |
| 1520-1545 |
FAST Integrator Presentation:
Structural Concept, Mr. Robert Biggs, Lockheed Martin |
| 1545-1610 |
Developing Reusable Launch Vehicle
Launch, On-Orbit and Reentry Safety Requirements, Mr. Edward
Browne, HQ AFSPC/SEC |
| 1610-1635 |
Innovation and Prototyping – A
Small Business Perspective, Mr. Mike Wolfert, Andrews Space |
Friday, 23
May 2008
|
| 0830-0900 |
Check in for the Tours |
| 0900 |
Bus Pickup for Tours |
| 0930-1130 |
Wind Tunnel Facilities Tour or
Structural Test Facilities Tour |
| 1200 |
Bus returns to Crowne Plaza |
*Agenda is subject to change
and is the most current available data to date. If you have
questions regarding the agenda, please contact
Cathy.Griffith@gdit.com
for more information.
Word documents of the RASTE agenda are available upon request. Please
contact
Jennie.Hempstead@gdit.com for a copy of the online agenda.
If you have any problems
accessing these pages, send an e-mail to
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