NASA Tests Alternate Launch Abort System For Astronaut Escape

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July 08, 2009

Grey Hautaluoma/Ashley Edwards 
Headquarters, Washington                                
202-358-0668/1756 
grey.hautaluoma-1@xxxxxxxx, ashley.edwards-1@xxxxxxxx 

Keith Henry                               
Langley Research Center, Hampton, Va.      
757-864-6120                          
h.k.henry@xxxxxxxx                      

Rebecca Powell 
Wallops Flight Facility, Wallops Island, Va. 
757-824-1139 
rebecca.h.powell@xxxxxxxx   
RELEASE: 09-156

NASA TESTS ALTERNATE LAUNCH ABORT SYSTEM FOR ASTRONAUT ESCAPE

WALLOPS ISLAND, Va. -- NASA has successfully demonstrated an alternate 
system for future astronauts to escape their launch vehicle. A 
simulated launch of the Max Launch Abort System, or MLAS, took place 
Wednesday morning at 6:26 a.m. at NASA's Wallops Flight Facility, 
Wallops Island, Va. 

The unpiloted launch tested an alternate concept for safely propelling 
a future spacecraft and its crew away from a problem on the launch 
pad or during ascent. The MLAS consists of four solid rocket abort 
motors inside a bullet-shaped composite fairing attached to a 
full-scale mockup of the crew module. 

The 33-foot-high MLAS vehicle was launched to an altitude of 
approximately one mile to simulate an emergency on the launch pad. 
The flight demonstration began after the four solid rocket motors 
burned out. The crew module mockup separated from the launch vehicle 
at approximately seven seconds into the flight and parachuted into 
the Atlantic Ocean. 

The test demonstrated a number of things: the unpowered flight of the 
MLAS along a stable trajectory; reorientation and stabilization of 
the MLAS; separation of the crew module simulator from the abort 
motors; and stabilization and parachute recovery of the crew module 
simulator. An important objective of the test was to provide the 
workforce of NASA's Engineering and Safety Center, or NESC, with 
experience in flight testing a spacecraft concept. NESC leads the 
project at NASA's Langley Research Center in Hampton, Va. 

NASA has chosen another launch abort system, known as the LAS, for the 
Orion spacecraft. The system has a single solid launch abort motor in 
a tower mounted at the top of the launch vehicle stack of the Orion 
and Ares I rocket. The LAS will be capable of automatically 
separating the spacecraft from the rocket at a moment's notice to 
make possible a safe landing. Orion, part of a new spacecraft system 
NASA's Constellation Program is developing, is undergoing design 
reviews in preparation for flying astronauts to the International 
Space Station in 2015 and, later, to the moon. 

Data from today's MLAS pad abort test could help NASA in several ways. 
MLAS is the first demonstration of a passively-stabilized launch 
abort system on a vehicle in this size and weight class. It is the 
first attempt to acquire full-scale aero-acoustic data -- the 
measurement of high loads on a vehicle moving through the atmosphere 
at high velocity -- from a faired capsule in flight. The test is also 
the first to demonstrate full scale fairing and crew module 
separation and collect associated aerodynamic and orientation data. 
In addition, data from the parachute element will help validate 
simulation tools and techniques for Orion's parachute system 
development. 

The NESC is an independently funded NASA program that draws on 
technical experts from across all NASA centers to provide objective 
engineering and safety assessments of critical, high risk projects. 

The MLAS is named after Maxime (Max) Faget, a Mercury-era pioneer. 
Faget was the designer of the Project Mercury capsule and holder of 
the patent for the "Aerial Capsule Emergency Separation Device," 
which is commonly known as the escape tower. 

NESC partners in the MLAS effort include Northrop Grumman Corporation. 


For images and video of the test firing, visit: 



http://www.nasa.gov/centers/wallops/missions/mlas.html 


For more information about NASA's Orion spacecraft and Constellation 
Program, visit: 



http://www.nasa.gov/constellation 

	
-end-



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