Well, at least it wasn't a frozen lox valve<https://groups.google.com/d/msg/sci.space/Cje3AmT5DUA/eqjPoa6Nx6sJ> . On Fri, Nov 22, 2013 at 1:05 PM, Ed Kelleher <Pres@xxxxxxxxxxxxxxxxxxxxx>wrote: > AW&ST and SpaceNews are reporting that SpaceX says their 2nd Stage Falcon > 9 reignition problem was due to frozen ignitor fluid lines. > > TEA freezes at 227K and TEB even colder than that, 180K. > > Has TEA/TEB ignition been used before on 2nd Stage? Seems most upper > stages are hypergolic, or augmented spark type ignition. > Apparently it hasn't been used much on American launchers. > > Ed Kelleher > > >