Exploration Systems Progress Report

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June 26, 2006

Dolores Beasley/Mike Braukus
Headquarters, Washington
Phone: (202) 358-1600/1979 

RELEASE: 06-249

EXPLORATION SYSTEMS PROGRESS REPORT

NASA engineers are in the midst of a new series of tests that will aid 
development of the agency's future space transportation systems. 

The tests support development and integration of the Crew Launch 
Vehicle, Crew Exploration Vehicle and Cargo Launch Vehicle under the 
Constellation Program. The program is developing both crew and launch 
vehicles for NASA's plan to return humans to the moon, Mars and 
destinations beyond. 

Since June, engineers at the Marshall Space Flight Center's 
Aerodynamic Research Facility in Huntsville, Ala., have conducted 80 
wind-tunnel runs on a partial model of the Crew Launch Vehicle. The 
model includes a portion of the upper stage, the spacecraft adapter, 
the Crew Exploration Vehicle and the launch abort system. The abort 
system is designed to lift the crew clear of the propulsion stack 
before or during launch in the event of an emergency. 

The tests use a 13-inch-long, 1.5 percent scale model in a 
14-by-14-inch cross section wind tunnel to simulate how proposed 
vehicle shapes perform in flight. In the test tunnel, giant fans or 
high-pressure air generate artificial wind that flows over 
scale-model vehicles, engines or rockets through a wide speed range. 
The tests are being conducted between Mach 0.8 and Mach 4.45, or 
about 600 to 3,300 miles an hour. Engineers use this flow 
visualization to analyze shock waves and flow expansion 
characteristics of components before their designs are incorporated 
into space hardware. 

This series is the latest step in a progression of wind tunnel tests 
that began in February. They are part of a coordinated partnership 
among NASA field centers and industry to set the foundation for 
design and development of the Crew Exploration Vehicle and Crew 
Launch Vehicle as an integrated system. This partnership includes 
Marshall; Langley Research Center, Hampton, Va.; Ames Research 
Center, Moffett Field, Calif.; and Boeing at St. Louis, Mo. 

Additional configuration tests are planned through July in the wind 
tunnel at Marshall. Those tests will serve as a foundation for more 
detailed launch vehicle design testing in the fall. 

Engineers at Marshall also have completed preliminary tests of an 
"augmented spark igniter," a critical engine component needed for 
in-flight ignition of liquid hydrogen and liquid oxygen propellants 
that mix and burn in engine combustion chambers. 

The test apparatus and a similar igniter will be used in development 
of the J-2X upper stage engine, an updated version of the powerful 
engine used to power the Saturn V rocket upper stages during the 
Apollo Program. The J-2X is planned for use in both the Crew Launch 
Vehicle's upper stage and the Cargo Launch Vehicle's Earth Departure 
Stage. The dual-use J-2X engine is an example of common hardware 
designed to simplify ground processing and reduce recurring operation 
costs. 

During the igniter tests, engineers integrated the igniter assembly - 
spark plugs, propellant injectors and tube-like ignition torch - and 
fired it into a vacuum chamber. This simulated the conditions the 
Crew Launch Vehicle's upper stage will experience when activated in 
low-Earth orbit. Future tests will chill propellants to minus 260 
degrees Fahrenheit prior to injection to simulate conditions between 
Earth and the moon, where the J-2X will be used to power the Earth 
Departure Stage. 

Preliminary analysis showed the test igniter operated as expected. 
Detailed analysis is continuing.

Crew Launch Vehicle and Cargo Launch Vehicle development efforts 
include multiple project element teams at NASA centers and contract 
organizations around the nation. These efforts are led by the 
agency's Exploration Launch Projects Office at Marshall. The office 
is part of the Constellation Program, hosted by NASA's Johnson Space 
Center, Houston. Constellation is a key program of NASA's Exploration 
Systems Mission Directorate in Washington. 

For information about NASA's exploration efforts on the Web, visit:

http://www.nasa.gov/exploration 

For information about NASA and agency programs on the Web, visit:

http://www.nasa.gov/home 

	
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