Bruno:
What I can talk about is the 2000 lbf thrust (at 600 psia) LR-101 which
weighes about 2 kg as a bare thrust chamber assembly and about 15 kg. as a
ready-to-install vernier engine. Both numbers are far heavier than would
be the case for a fixed engine. Perhaps those who have flown one can
comment on as-flown weights.
Bill
On Sunday, August 7, 2016, Bruno Berger <mailinglists@xxxxxx> wrote:
Does anybody have an idea what the mass of Rocket Lab's Rutherford
engine is (with or without pump assembly)? Or any other engines in a
similar thrust range (5-6 klbs)
Thanks!
Cheers Bruno
--
Bruno Berger
Swiss Propulsion Laboratory
E-Mail: bruno.berger@xxxxxx <javascript:;>
PGP key: http://www.spl.ch/contact/Bruno.Berger.asc
WWW: http://www.spl.ch
