Ares 1 marches (or staggers) on:
Thrust Oscillation is specifically named in relation to end of the first stage burn of Ares I-X, which requires mitigation – proposed to be in the form of high strength fasteners.
“Preliminary results show lower axial loads and higher lateral loads during thrust oscillation at the end of the FS (First Stage) burn (T+120sec). Proposed mitigation (high strength fasteners in impacted hardware) in work, needs to be presented at ERB (Engineering Review Board).
Afraid it will shake apart? Use bigger screws!
I love this, too.
While beefing up the structure is a mitigation for the hardware, Ares I-X’s components are also in the TO firing line, with the most concerning element referencing the Flight Termination System (FTS) – which may require a range waiver due to the potential TO could exceed the components certification, and the threat of vibrating them out of action.
“Requirement – Range Safety: multiple waivers. Lack of dual S&A device. Lack of initiation of LSC at both ends. Lack of “CRD Self-test” capability. Minimum separation of FTS components,” added the presentation.
We may massage the thing so hard that we won’t be able to blow up the vehicle if something goes wrong (e.g., it starts blasting toward the VAB). Can we have a waiver, please?
NASA’s unending ability to waive itself from its own requirements is one of the reasons that the notion of “human rating” is nonsensical.
[Early evening update]
Link to NASA Space Flight was bad before. It’s fixed now. I’m kind of surprised that it took all day for someone to point it out. Just more evidence that most people don’t follow the links, at least if I post significant excerpts and/or commentary on them.
[Update a couple minutes later]
Rob Coppinger has Ares 1, then and now. That upper stage has really grown. I also hadn’t realized that it had a common bulkhead for the tanks. Well, at least it’s not hypergolic.