Pistonless pump


A Pistonless pump is a type of pump designed to move fluids without any moving parts other than three chamber valves.
The pump contains a chamber which has a valved inlet from the fluid to be pumped, a valved outlet - both of these at the bottom of the pump, and a pressurant inlet at the top of the pump. A pressurant is used, such as steam or pressurized helium, to drive the fluid through the pump.

Introduction

NASA have developed a Low cost rocket fuel pump which has comparable performance to turbopump at 80-90% lower cost. Perhaps the most difficult barrier to entry in the liquid rocket business is the turbo pump. A turbo pump design requires a large engineering effort and is expensive to manufacture and test. Starting a turbo pump fed rocket engine is a complex process, requiring a careful synchronisation of many valves and subsystems. In fact, Beal aerospace tried to avoid the issue entirely by building a huge pressure feed booster. Their booster never flew, but the engineering behind it was sound and, if they had a low cost pump at their disposal, they might be competing against Boeing. This pump saves up to 90% of the mass of the tanks as compared to a pressure fed system. This pump has really proved to be a boon for rockets. By using this pump the rocket does not have to carry such a heavy load and can travel with very high speed.

Working cycle

The cycle is as follows:
Rocket engines requires a tremendous amount of fuel
at high pressure. Often the pump costs more than the thrust
chamber. One way to supply fuel is to use the expensive
turbopump mentioned above, another way is to pressurize fuel
tank. Pressurizing a large fuel tank requires a heavy, expensive
tank. However suppose instead of pressurizing the entire tank, the
main tank is drained into a small pump chamber which is then
pressurized. To achieve steady flow, the pump system consists of
two pump chambers such that each one supplies fuel for half of
each cycle. The pump is powered by pressurized gas which acts
directly on the fluid. For each half of the pump system, a chamber is
filled from the main tank under low pressure and at a high flow
rate, then the chamber is pressurized, and then the fluid is
delivered to the engine at a moderate flow rate under high
pressure. The chamber is then vented and cycle repeats. The
system is designed so that the inlet flow rate is higher than the
outlet flow rate. This allows time for one chamber to be vented,
refilled and pressurized while the other is being emptied. A bread
board pump has been tested and it works great. A high version
has been designed and built and is pumping at 20 gpm and 550 psi.

Application in rocketry

It is most commonly used to supply propellants to rocket engines. In this configuration there are often two pumps working in opposite cycles to ensure a constant flow of propellants to the engine.
The pump has the advantage over a pressure-fed system in that the tanks can be much lighter. Compared to a turbopump the pistonless pump is a much simpler design and has less stringent design tolerances.

Advantages

Nearly all of the hardware in this pump consists of pressure
vessels, so the weight is low. There are less than 10 moving parts,
and no lubrication issues which might cause problems with other
pumps. The design and construction of this pump is straight forward and no
precision parts are required. This device has advantage over standard
turbopumps in that the weight is about the same, the unit, engineering and test
costs are less and the chance for catastrophic failure is less. This
pump has the advantage over pressure fed designs in that the weight of
the complete rocket is much less, and the rocket is much safer
because the tanks of rocket fuel do not need to be at high pressure. The
pump could be started after being stored for an extended period with
high reliability. It can be used to replace turbopumps for rocket
booster option or it can be used to replace high pressure tanks for deep
space propulsion. It can also be used for satellite orbit changes and
station keeping.

Disadvantages

The pistonless pumps has disadvantages along with such fine advantages.
  1. They cannot pump to higher pressure than drive gas
  2. They cannot use either a staged combustion or expander cycle.
  3. A gas generator cycle is also difficult to integrate with the pistonless pump.
  4. The generated gas must be chemically compatible with both the propellants.
  5. This gas generator lowers the Ignition start period of the engine.