MiG-21 Fuel System
The described fuel system is the one of the MiG-21US (Type 68, NATO Mongol B). However, it is very similar to the one used in
MiG-21PF, MF, BIS except for differences in fuel quantity and annunciator light markings. I'll add the missing schematic at a later time.
Definitions:FT - Fuselage Tank
BDT - Belly Drop Tank
WT- Wing Tank
The fuel system consists of six FT's, four integral WT's, one BDT. The fuel tanks (No. 2 to No. 7) are located between bulkheads No. 7 and No. 28. They are made from two soft layers except for
tank No. 7. The inner layer is from fuel-resistant rubber of 0.5 mm thickness and outer one is from rubberised fabric of l.l-29.5mm thickness. These "soft" tanks are located in special metal boxes.
The fuel system consists of two sub systems, these being the
pressurization system and a control pressure system.
The pressurization system consists of a compressed bleed air
which is fed to each of the eleven tanks. The pressure
varies from tank to tank, highest pressure being bled to the
BDT followed by the WT's and the FT's respectively. The system works under the principal that the fuel under
highest pressure is transferred first. Two auxiliary fuel
pumps are present in FT-3 and FT-4 and fuel flow is aided by
an engine driven fuel pump tanks FT-1 and FT-3 are key to
the operation of the system, FT-1 being a flow control unit
and Ft-3 being the only tank from which fuel is transferred
directly to the engine.
OPERATION and WORKING PRINCIPAL
The system pressurizes itself as soon as engine bleed air is
present and initial fuel (about 70...100 liters) is taken
only from Group-2 (FT-1...3). FT-1 incorporates
pressurization float valves (#10, 11) which activate the
fuel cock (13) as soon as fuel level in FT-1 drops 70...100
liters. The fuel cock is opened by the pressure control
system which is directly linked to float valves. This sub
system consists of a series of pressure lines which sense
changing pressure at the float valves thereby controlling
fuel transfer from the WT's and the BDT. The highest pressure is bled to the BDT thereby being the first tank consumed. Once empty fuel is transferred from the
WT's to FT-3. This is accomplished by bleeding the next
lowest pressure to the wing tanks. Fuel the flows through
check valves (9) to the fuel cock (13) into FT-2,
transferred to FT-3 and then pumped to engine. The
consumption of fuel contained in Group-3 (FT-4...6) occurs
in much the same way as the WT's except that transfer to FT-
3 is aided by an auxiliary fuel pump (5). Safety features include a network of overflow lines connecting Group-2,3, WT's and the BDT. The pressure
limiters are also incorporated to prevent overboosting of
the system. Emergency jettison of the BDT is done
pyrotechnically.
SEQUENCE OF FUEL CONSUMPTION |
| Fuel at Gauge | annunciator lights |
drop tank | 2200...2350 liters | drop tank empty |
3. group | 750..850 liters | 3. group empty |
Reminder | 400...500 liters | 500 liters remaining |
REMARKS / EMERGENCY PROCEDURES
...If "Group 3 Empty" already lights at 1300...1400 Liters
means some trouble with the WT's. Actual fuel remaining for
use is 170...850 Liters. Go to land and consider a higher
weight due to the still full WT's. ...If one of the pump annunciator lights at a higher
quantity than shown above, always check the
switches. Afterburner-use with Main Pump in Off position
can cause engine failure. ...In case of landing with fuel remaining of less than 200
Liters (52 Gallons) the "pump of group 3" should be on to
use eventual unused fuel still in Group 3. The pump should
work until the landing has been accomplished in this case...Flashing of the light "Main Pump" at altitudes higher
than 45000 ft:
1. disengage afterburner; military power only!
2. rapidly descent below 45000 ft; then decrease power for
further descent
3. Approach Airport for landing at 15000 ft or less
4. do not apply negative G-load