Orbital ATK, NASA Report Initial Findings From Qualification Motor (QM-1) Test | Aero-News Network
Aero-News Network
RSS icon RSS feed
podcast icon MP3 podcast
Subscribe Aero-News e-mail Newsletter Subscribe

Airborne Unlimited -- Most Recent Daily Episodes

Episode Date

Airborne-Monday

Airborne-Tuesday

Airborne-Wednesday Airborne-Thursday

Airborne-Friday

Airborne On YouTube

Airborne-Unlimited-04.29.24

Airborne-NextGen-04.30.24

Airborne-Unlimited-05.01.24 Airborne-AffordableFlyers--05.02.24

Airborne-Unlimited-05.03.24

Wed, May 13, 2015

Orbital ATK, NASA Report Initial Findings From Qualification Motor (QM-1) Test

Successful Orbital ATK Five-segment Motor Qualification Test Demonstrates Progress On NASA’s Space Launch System

Data from the first five-segment qualification motor (QM-1) test conducted by Orbital ATK and NASA show the solid rocket motor performed as designed. Manufactured by Orbital ATK, the five-segment motor will be used to provide liftoff and ascent thrust for NASA’s Space Launch System, or SLS.

“Having analyzed the data from QM-1 for a little more than a month, we can now confirm the test was a resounding success,” said Charlie Precourt, Vice President and General Manager of Orbital ATK’s Propulsion Systems Division, and four-time space shuttle astronaut. “These test results, along with the many other milestones being achieved across the program, show SLS is on track to preserve our nation’s leadership in space exploration.”

NASA’s SLS will launch on its first mission, Exploration Mission-1, in just a few years. The SLS vehicle, along with NASA’s Orion crew capsule, will take humans farther into space than ever before.

The QM-1 static test had 102 design objectives and was supported by more than 530 instrumentation channels. A key objective of QM-1 was to test the solid rocket motor performance at high temperature (90 degrees F mean bulk temperature). Current data show the nozzle and insulation performed as expected, and ballistics performance parameters met allowable requirements. Additionally, the thrust vector control and avionics system provided the required command and control of the motor nozzle position.

Orbital ATK’s new five-segment boosters for SLS leverage a flight-proven four-segment design, while implementing technological and performance upgrades including: the addition of a fifth motor segment to provide increased power, an advanced avionics system, a more environmentally friendly motor insulation design, a safer flight termination system, and more efficient and modern processing techniques. These changes were designed to meet performance requirements and increase reliability, while lowering manufacturing costs.

This first test of the SLS qualification phase of testing (QM-1) was preceded by a robust three-test demonstration phase (DM-1, DM-2 and DM-3) that helped to substantiate motor design. The qualification phase will conclude with QM-2, scheduled for next spring, fully demonstrating the motor’s readiness for flight. QM-2 will test the motor performance at the lower temperature limit (40 degrees F), whereas QM-1 tested the upper temperature limits (90 degrees F).

“Ground tests are very important – we strongly believe in testing before flight to ensure lessons-learned occur on the ground and not during a mission,” said Precourt. “With each test we have learned things that enable us to modify the configuration to best meet the needs for the upcoming first flight.”

The next major milestones for SLS include further Boeing core stage development and testing at NASA’s Michoud Assembly Facility, continued testing of Aerojet Rocketdyne’s RS-25 engine at NASA’s Stennis Space Center, and avionics and controls testing at Marshall Space Flight Center.

(Image provided by Orbital ATK)

FMI: www.orbitalatk.com

Advertisement

More News

ANN's Daily Aero-Linx (05.02.24)

Aero Linx: Model Aeronautical Association of Australia MAAA clubs are about fun flying, camaraderie and community. For over 75 years, the MAAA has been Australia’s largest fl>[...]

ANN's Daily Aero-Term (05.02.24): Touchdown Zone Lighting

Touchdown Zone Lighting Two rows of transverse light bars located symmetrically about the runway centerline normally at 100 foot intervals. The basic system extends 3,000 feet alon>[...]

Aero-News: Quote of the Day (05.02.24)

“Discovery and innovation are central to our mission at Virgin Galactic. We’re excited to build on our successful record of facilitating scientific experiments in subor>[...]

ANN FAQ: Contributing To Aero-TV

How To Get A Story On Aero-TV News/Feature Programming How do I submit a story idea or lead to Aero-TV? If you would like to submit a story idea or lead, please contact Jim Campbel>[...]

NTSB Final Report: Cirrus Design Corp SR20

Student Pilot Reported That During Rotation, “All Of A Sudden The Back Of The Plane Kicked To The Right..." Analysis: The student pilot reported that during rotation, “>[...]

blog comments powered by Disqus



Advertisement

Advertisement

Podcasts

Advertisement

© 2007 - 2024 Web Development & Design by Pauli Systems, LC