[AR] Re: LOX/kero layout (was Re: Above 65000 ft for free)

  • From: Peter Fairbrother <zenadsl6186@xxxxxxxxx>
  • To: arocket@xxxxxxxxxxxxx
  • Date: Thu, 6 Sep 2018 20:47:40 +0100

On 04/09/18 08:17, Wyatt Rehder wrote:

Also at 400N I'm not sure a turbopump would be the most efficient
choice. Far as I knew they don't scale down to sizes that small that
well.

They do not, which is why I have been working on exotic materials for blisks.

However if you don't want RD-170 (or BE-4) numbers something like below can be done.

With a turbine inlet temperature of only 600C and a tip speed of 275m/s, the turbine material requirement isn't too ridiculous, and the overall turbopump efficiency requirement is only 10.0%.

However ... that 10% efficiency is not easily obtained.

Pump specific speeds are about 150-600 (US units) - Barske pumps can deliver about 15-40% efficiency in that range, if well designed and built. Turbine efficiencies of about 60% are also attainable, and 80% plus mechanical linkages are possible.

However you have to match the turbine and the pumps for torque and speed, which is not easy, an even then - 15% x 60% x 80% = 7.25% = fail.



But do I think it is doable :)


Peter Fairbrother



400N rocket engine v2.0

LOX-rich staged combustion

Pumps:

LOX - 107 g/s   @ 1.142 kg/l    = 93.7 ml/s
kero - 45 g/s   @ 0.78  kg/l    = 57.7 ml/s
total = 152 g/s                 = 151.4 ml/s
O/F = 2.38

output pressure 12 MPa

delivered power LOX     1125W   (93.7 ml/s x 12MPa)
delivered power RP1      693W   (57.7 ml/s x 12MPa)
delivered power total   1818W

at 100,000 rpm-
LOX head= 1050m 93.7 ml/s specific speed = 166 (= 291 US units)
kero head= 1538m 57.7 ml/s specific speed = 97  (= 163 US units)

at 200,000 rpm-
LOX head= 1050m specific speed = 332 (= 582 US units)
kero head= 1538m specific speed = 194 (= 326 US units)


Preburner:

11.6 MPa -> 6MPa exit
LOX/RP1 O/F 36:1
Ae/At 1.0046
Te 613C, 886K
Ve 573 m/s  mach 1.07  26.1 kg/m^3
110 g/s flow rate


Turbine:

Gas stream kinetic power 18.06kW
Pumps delivered power   1818W
Turbopump overall efficiency required 10.0%

20 degree Turbine tip optimum velocity 275 m/s



Main Chamber:

Pc 6MPa  Pe 1 atm
LOX/RP1 2.38
Ae/At 9.09
ISP: 295s 321s(vac)


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