TechNews logo

Milestone for Ares I Vehicle

Published Thu, 2007-01-04 23:48

NASA has completed the Ares I crew launch vehicle system requirements review. The review brings the agency one step closer to developing a new mode of space transportation for astronauts on missions to explore the moon, Mars and other destinations.

The system requirements review confirmed that the Ares I system requirements were complete, validated and responsive to mission requirements.

It also confirmed that the Ares I architecture and design concept can fulfill the mission objectives and that the Ares project is ready to begin engineering design activities. The Ares preliminary design review is scheduled for mid-2008.

This review is the first in a series of milestones that will occur before the actual flight hardware is built. Each major review provides more detailed requirements for the vehicle design to ensure the overall system can meet all NASA requirements for safe and reliable flight. The review process also identifies technical and management challenges, and addresses ways to reduce potential risks as the project goes forward.

Among the items addressed in the review was the commitment to reduce operations costs through streamlined launch vehicle processing. All hardware elements -- the first stage, upper stage and upper stage engine -- are emphasizing operations simplicity to enable NASA to sustain long-term exploration of space within its budget.

The review follows a series of successful system requirements reviews for the Ares launch vehicle project, including for the J-2X engine, Ares I first stage and Ares I-1 test flight. The J-2X engine will power the upper stage of Ares I, as well as the Ares V Earth departure stage that will propel Orion from Earth orbit to the moon late next decade. Ares I-1, planned for launch in 2009, will be the first test flight of the integrated launch vehicle system.

In January 2007, the Ares project will begin the second in a series of design analyses cycles leading to final design and fabrication of the launch vehicle. This cycle will baseline design changes made during the first cycle. In the updated Ares 1 configuration, a common bulkhead between the upper stage liquid hydrogen and liquid oxygen tanks has been substituted for an intertank, thus shortening the vehicle. The thrust profile for the Ares I first stage also has been baselined. This means requirements have been established for how the solid propellant inside the five-segment reusable solid rocket booster burns during ascent.


Post new comment

The content of this field is kept private and will not be shown publicly.