S
SpaceKiwi
Guest
Just read the article on SDC confirming the fact that the Delta-4 Heavy's problem was propellant vaporization in the fuel line.<br /><br />I've got to ask what is this continued insistance in the space business of engine performance being rated at greater than 100%? Surely an engine develops a certain amount of thrust/speed/whatever with the 'throttle' opened right up, and that maximum developed 'grunt' should be identified as pedal-to-the-metal, goin'-like-the-clappers, flat-out-with-a-tail-wind 100% performance?!<br /><br />Also, with respect to the Delta problem, why the need to computer-control shut down the engines in a 'dry' situation? Wouldn't the dry line into the chamber make this redundant anyway? <div class="Discussion_UserSignature"> <p><em><font size="2" color="#ff0000">Who is this superhero? Henry, the mild-mannered janitor ... could be!</font></em></p><p><em><font size="2">-------------------------------------------------------------------------------------------</font></em></p><p><font size="5">Bring Back The Black!</font></p> </div>