nu kaip adaptuotam įmesiu, pats matau nesugebi rast. newsų Ciolkovskis 
ble :D

  The launcher's central kerosene tank is surrounded on four sides and 
the top by liquid oxygen tanks; the liquid nitrogen tank is nearby at 
the bottom. The kerosene tanks of the four boosters are relatively small 
and compact, and also between a liquid oxygen and a liquid nitrogen 
tank. Thus, once the kerosene was chilled initially, it could remain so 
for the brief time needed to finish launch preparations. The latest 
version of Falcon 9, Falcon 9 Full Thrust also has the capability of 
sub-cooling the RP-1 fuel to −7 °C, giving a 2.5–4% density increase.

2018.02.10 23:14, js rašė:
> Ne aie tai dunduk tu ble.
> Tu sakai kad raketoje kazkas saldo pati kura.
> Imesk schema arba kur parasyta apie sita procesa.
> 
> 
> 
> 10.02.2018 23:09, Dainiushas rašė:
>> jau net nejuokinga, wikipediją uždarė?
>>
>> First stage
>> Engines    9 Merlin 1D
>> Thrust    Sea level: 7.6 MN (1,700,000 lbf)
>> Vacuum: 8.2 MN (1,800,000 lbf)
>> Specific impulse    Sea level: 282 seconds
>> Vacuum: 311 seconds
>> Burn time    187 seconds
>> Fuel    Subcooled LOX / Chilled RP-1
>>
>> 2018.02.10 22:48, js rašė:
>>> Imesk schema ar linka kur raketoje saldo zibala
>>>
>>> 09.02.2018 9:04, Dainiushas rašė:
>>>> žibalą šaldo gi.
>>>>
>>
>