The NASA docs posted some pages back point out some crucial details worth noting.
Adding more rotors (eg tail to 5) and having certain non-uniform angles can depending on the airframe result in audio profile reductions of up to 10db (in the public data PDF) in the crucial up-range approach at the cost of deceased load/range. We've seen that the tail had 5+ blades, and quite feasibly irregularly spaced angles. NASA's opinion is that the same can be done to the main rotor, but unfortunately we don't have pics of it, and *if* bits were left (BHD site et al) it would probably be difficult to determine blade angle with a stealth fairing and/or ashes.
There's really only two mechanical engineering reasons why it might not be a mod kit tail for XH-60BDP:
- There's no destinctive H-60 'blister' at the top of the tail, meaning that portion of the mechanics is radically different.
- The tail stabs can't join like a normal H-60 due to the elongated fairing (rather large for just LoDrag, ECM maybe?) so the stab controls (which could fit inside the fairing) would need a custom rocker arm or something new to actuate.
BTW, one of the news pics, Wall Street Jounal set iirc, shows some skid lines or something indicating that the stabs are not fixed, but are intended to rotate. +1 for H-60 there.
Now as for the mechanical failure, the rumormongers said it was having mech problems inbound but not due to hostile fire. A speculative possibility is that the lift effect harmonic of an irregularly spaced main rotor caused problems, or stalled on the wall or any of the other common maladies associated with 'flight' by beating the air into submission.