Infrasonic Characterization of the Falcon Hypersonic Technology Vehicle (HTV-2) Test Advanced Technologies Enabling Long-Duration Hypersonic Flight for Prompt Global Reach Rob Davies, USARPAC Frank Highsmith, USPACOM Chris Gastion (Kwajelein), AFTAC/DIA Dr. John Olson, Geophysical Institute, Univ Alaska, Fairbanks Jay Helmericks, Geophysical Institute, Univ Alaska, Fairbanks 5-14 Aug 2011
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Infrasonic Characterization of the Falcon Hypersonic Technology Vehicle
(HTV-2) TestAdvanced Technologies
Enabling Long-Duration Hypersonic Flight for Prompt Global Reach
Rob Davies, USARPAC Frank Highsmith, USPACOM
Chris Gastion (Kwajelein), AFTAC/DIADr. John Olson, Geophysical Institute, Univ Alaska, FairbanksJay Helmericks, Geophysical Institute, Univ Alaska, Fairbanks
5-14 Aug 2011
2
HTV-2A Planned Mission Trajectory and Timeline
3
HTV-2 External Configuration
0.5 inch R leading edges
Elliptic nose
Wing Sweep Break point
GPS Frustum-AntennaCLS Antenna
S/C Band Antenna (2)
Windward slice
Split-windward flaps
Reaction Control System
GPS Aft-Antenna
Plasma Probe
4
HTV-2A Flight Path & other Assoc. Ops
33.8 N, 147.1 W
26.2 N, 152.1 W
20.8 N, 169.2 W
17.6 N, 177 W
12.6 N, 176.7 E
Pacific Collector
OTTR-
OTTR
Worthy
TSP 5
TSP 4
TSP 3
TSP 2
TSP 1
Pacific Collector
OTTR
Makaha Ridge
MATSS
OTTR
Worthy
Roi-Namur
G-III
Cast Glance
BH-341
Tern Island chosen due to it’s proximity to flight path
French Frigate Shoals
Distribution authorized to U.S. Government Agencies only
MDA Associate Operations
Radars AEGIS - 1 AEGIS DDG located N. of Hawaii AN/TPY - 1 system located at VAFB tracking booster fly-
out SBX – North of Hawaii GBR-P – RTS
Electro-Optic/IR WASP - Modified DC-10, Vis, NIR, MWIR, LWIR, observe