![]() |
#3
|
|||
|
|||
![]() Damon Hill wrote: I'd imagine something like the burner/turbine section of a turbojet; one turbopump assembly for each F-1 engine. There are a number of engine designs that use multiple combustion chamber/nozzles per turbopump. Others have a separate gas generator/turbopump for both the oxidizer and fuel; the tradeoffs are various. Info on and cutaways of the engine he http://history.nasa.gov/SP-4206/ch4.htm#117 Pat |
Thread Tools | |
Display Modes | |
|
|
![]() |
||||
Thread | Thread Starter | Forum | Replies | Last Post |
How are rocket engine pumps powered ? | Andre Majorel | History | 11 | October 13th 07 08:30 PM |
Challanger Turbo Pumps? | Danny Dot | Space Shuttle | 0 | September 8th 06 09:51 PM |
Pressure fed rockets and cheap pumps | Larry Gales | Technology | 0 | November 14th 03 04:42 AM |
Pressure fed rockets and cheap pumps | Larry Gales | Policy | 0 | November 14th 03 04:42 AM |
inefficient turbo-pumps and Isp | Greg | Technology | 10 | August 25th 03 09:33 PM |