ALV X-1

infobox rocket
name = ALV X-1
imsize = 300

---

caption = ATK ALV X-1 Launch Vehicle Pathfinder
function = Sub-Orbital Test Vehicle
manufacturer = Alliant Techsystems
country-origin = United States
height = 54 feet
diameter = 5 feet
mass = Unknown
sites = Mid-Atlantic Regional Spaceport
status = Inactive
stages = 2
launches = 1
fail = 1

ALV X-1 was to be a sounding rocket flight of a vehicle developed by Alliant Techsystems called the ATK Launch Vehicle (ALV). The rocket carried the SOAREX-VI and Hy-BoLT experiments as payloads.cite web |url=http://atk.mediaroom.com/index.php?s=press_releases&item=626 |title=ATK Completes Successful Pathfinder for Its New Launch Vehicle |date=2006-10-10 |publisher=ATK] The flight was launched at 09:10 GMT on 2008-08-22, and then the rocket was intentionally destroyed 20 seconds into flight after veering too far off course. [cite web |url=http://hamptonroads.com/2008/08/rocket-explodes-shortly-after-launch-wallops-island|first=Cindy|last=Clayton|title=Rocket explodes shortly after launch at Wallops Island|date=2008-08-22|accessdate=2008-08-22|language=English|publisher=Pilot Online] Launch occurred from LP-0B at the Mid-Atlantic Regional Spaceport (MARS) at NASA's Wallops Flight Facility.

Hy-BoLT

The Hypersonic Boundary Layer Transition (Hy-BoLT) experiment payload was sponsored by the Hypersonics Project within the Fundamental Aeronautics Program of NASA. Hy-BoLT was a wedge-shaped payload that would have provided "valuable data on the fundamental physics of high-Mach flight."cite web |url=http://www.airspacemag.com/flight-today/hypersonics.html |title= Mach 20 or Bust |last=Little |first=Geoffrey |date=2007-09-01 |publisher=Air & Space Magazine] It would have been launched to an altitude of mi to km |250 |precision=-1, transmitting various temperatures and pressures on different parts of the vehicle's surface.

During the flight, Hy-BoLT transmitted data as expected for the first 20 seconds until it was destroyed when the rocket was detonated.

SOAREX-VI

Sub-Orbital Aerodynamic Re-entry EXperiments VI (SOAREX-VI) was sponsored by the Hypersonics Project within the Fundamental Aeronautics Program of NASA, and developed by NASA's Ames Research Center. It was carried by the ALV X-1 as a secondary payload. SOAREX-VI would have attempted to characterize an innovative self-orienting reentry vehicle shape called the Slotted Compression RAMP (SCRAMP) probe. The SOAREX-VI package also included an atmospheric density calibration probe built by NASA Ames in cooperation with the University of Idaho, and an AIS probe built by the United States Naval Research Laboratory (NRL).

After detonation of the rocket, the SOAREX-VI enclosure inside was broken open. The SCRAMP probe, designed to activate upon ejection, did exactly that and acquired two TDRSS satellites overhead and an S-band tracking dish on land. It transmitted sensor and video data until it was destroyed on splashdown.

References

See also

* Boeing X-51
* Force Application and Launch from Continental United States
* HyShot
* NASA X-43
* Operationally Responsive Space Office

External links

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