"Hey Ed,<br /><br />Since you are in the insurance business, do you know what % of cost of a launch vehicle is incurred by the engines?<br /><br />I've been told it's approx. 30%, but figure a insurance man probably will have better data"<br /><br /><br />I am frequently hired by insurance adjustors as an engineering consultant, but I'm also hired by non-insurance types so I don't think of myself as being "in" the insurance business. But I do have some numbers on hand that address your question. The answer, of course, is that it depends. <br /><br />Take Atlas V-401 and Delta IV Medium as examples. Scribbles in my weathered space stuff notebook tell me that an RD-180 may cost $12 million or more, an RS-68 $14 million, and an RL10 something like $6.5 million. Other notes say that an Atlas V-401 launch, including all of the launch services, costs $136 million and that a Delta IV Medium might cost about the same. For these two examples then, the main propulsion costs are roughly 14% (Atlas V) and 15% (Delta IV) of the total price. <br /><br />OTOH, a higher-thrust LEO version of Atlas V (402 with two RL10s) would have a propulsion cost percentage of more than 17%, while a Delta IV Heavy might be something like 20%, etc.. Solid rocket motors would also have an effect on the propulsion cost percentage.<br /><br /> - Ed Kyle