While the design lacks complicated turbopumps and cryogenic fuels, it does have one drawback: the N2O is contained in a pressure vessel. If that tank is damaged while still full (or close to), bad things can happen.
While the design lacks complicated turbopumps and cryogenic fuels, it does have one drawback: the N2O is contained in a pressure vessel. If that tank is damaged while still full (or close to), bad things can happen.
http://www.knightsarrow.com/rockets/scaled-composites-accide...
http://www.dtic.mil/dtic/tr/fulltext/u2/a489459.pdf
(In that Air Force research lab report there's mention of supercritical N20 causing a spontaneous explosion with coffee grounds.)
Strong oxidizers are almost universally hard to handle. About the nicest ones around are Lox, Nox and hydrogen peroxide.
Don't forget that this is not the first fatality associated with this engine. In 2007, 3 people were killed in an explosion during a static test at Mohave Air & Space port.
Is this a case of not seeing safety's big picture? Cutting accidents in half (or by whatever) is great, but not if that means the remaining accidents are fatal. A more frequent controlled failure is a much better scenario, but I imagine hurts the bottom line too much.
I'm wary that for-profit companies aren't going to invest enough in private manned spaceflight's safety when there's a profit incentive at work dictating otherwise. At least without a fair bit of regulation.