3.3.24 · D1Rocket Propulsion

Foundations — Expander cycle — hydrogen-cooled nozzle drives turbine

2,549 words12 min readBack to topic

Before we can talk about turbines and cooling channels, we need a shared vocabulary. Every symbol below is a measurement of the moving fluid. We build them one at a time, each on top of the last.


1. Flow: what "moving fluid" even means

The picture. Imagine a pipe. Draw an imaginary flat window across it. Count the mass of fluid that pushes through that window in one second — that count is . The little dot on top is standard notation for "per second" (a rate).

Figure — Expander cycle — hydrogen-cooled nozzle drives turbine

Why the topic needs it. Every energy quantity in the parent note is a rate — heat per second, work per second (that is, power). To get a rate of energy you always multiply an energy-per-kilogram by . So is the bridge between "per kilogram" facts and "per second" facts.

Recall

What does the dot in mean? ::: "per second" — it makes a rate.


2. Pressure — how hard the fluid pushes

The picture. Squeeze a balloon: the air inside pushes back equally on every part of the skin. That push-per-area is pressure. In a rocket chamber the burning gas pushes outward at ~ — about 100 times atmospheric.

Why the topic needs it. A pump's whole job is to raise pressure so fuel can be forced into the high-pressure chamber. We write that rise as (Greek capital delta = "the change in"). A turbine does the opposite: it lets pressure fall and harvests the released energy. So pressure — and its rise/fall — is the currency of the whole cycle.


3. Density — how tightly packed

The picture. A cubic metre of liquid oxygen weighs ; the same box of liquid hydrogen weighs only . Oxygen is dense, hydrogen is fluffy.

Why the topic needs it. A pump handles volume, but we track mass. Density converts between them: volume flow . This single fact is why the parent note says the oxygen pump is "cheaper" — dense oxygen means small volume per kilogram, so less work to push it. Light hydrogen means large volume per kilogram, so a hungrier pump. See Liquid hydrogen properties.

Figure — Expander cycle — hydrogen-cooled nozzle drives turbine
Recall

Volume flow in terms of and ? ::: (kilograms-per-second divided by kilograms-per-cubic-metre gives cubic-metres-per-second).


4. Temperature and its change

The picture. Cold H₂ enters the wall channels; the flame outside pumps heat into it; it leaves hotter. The rise is .

Why the topic needs it. The entire trick of the cycle is that heat raises the hydrogen's temperature. How much heat per kelvin depends on the next symbol.


5. Specific heat (and its partner )

Why this tool, and not something simpler? We need a bookkeeping number that turns "how many degrees hotter" into "how many joules absorbed." That is exactly what is defined to be. So the heat rate follows directly:

Read left to right: (kilograms per second) × (joules per kg per kelvin) × (kelvin) = joules per second = watts. Every unit cancels perfectly into power.

The picture. Think of each kilogram as a bucket. is the bucket's size: hydrogen's bucket is huge (14 000 J per degree), so a little mass soaks up a lot of heat. That is why only hydrogen makes this cycle work — see the Regenerative cooling jacket where all this heat is grabbed.


6. Enthalpy — the gas's usable energy content

The picture. Picture the hot gas as a loaded spring plus its heat. As it flows through the turbine and its temperature drops from to , the enthalpy drops too, and the released energy spins the blades.

Why the topic needs it. Turbine work per kilogram is the enthalpy drop, . Multiply by to get power. This is the direct link from "heat we stole" (Step 1) to "power we make" (Step 2). For the deeper flow relations see Isentropic flow relations.


Why this tool? When a gas expands smoothly and without leaking heat (an "isentropic" expansion — a clean, ideal one; here again the ideal-gas assumption of §6 is in force), its temperature and pressure are locked together by

We need this because a turbine is driven by a pressure drop, but the energy it releases is a temperature drop. is the exact conversion knob between the two. Without it we could not turn "pressure fell from to " into "here is how many degrees it cooled, hence how much power came out."

The picture. Steeper pressure fall → steeper temperature fall → more work. The exponent (about for ) controls how steep.

Figure — Expander cycle — hydrogen-cooled nozzle drives turbine
Recall

What links the temperature ratio to the pressure ratio in a clean expansion? :::


8. Efficiency — the "real machines waste some" factor

Why it matters here. Turbines multiply by (you get less than ideal). Pumps divide by (you must supply more than ideal). Both push the self-sustaining balance closer to failure — the cycle only "closes" if the turbine, after its losses, still beats the pumps, after theirs. See Turbopump design.


9. Putting symbols into the two work formulas

Now that every symbol is defined, we can write the two expressions the parent note bookkeeps.


How it all feeds the cycle

Read each node as the symbol it stands for: m-dot is , cp is , delta-T is , Q is the heat rate, h is enthalpy, gamma is , p is pressure, rho is , delta-p is , eta-t and eta-p are the two efficiencies, and the two W nodes are turbine and pump power.

m-dot = mass flow

Q = heat rate

cp = specific heat

delta-T = temp rise

h = enthalpy

T = temperature

cv = const-volume heat

gamma = cp over cv

pressure-temperature link

p = pressure

W-turb = turbine power

eta-t = turbine efficiency

W-pump = pump power

delta-p = pressure rise

rho = density

eta-p = pump efficiency

self-sustaining condition

Read it top-down: the raw measurements (mass flow, specific heat, temperature) build the heat rate and enthalpy; and build , which with pressure builds the turbine's expansion; density and build the pump demand; efficiencies trim both; and everything meets at the single inequality that decides whether the engine can power itself.


Equipment checklist

Cover the right side and test yourself — you are ready for the parent note only if each comes instantly.

means
mass flow rate, kilograms passing a point per second.
and mean
pressure (force per area, in Pa) and its change; for a pump .
means
density, mass per cubic metre; converts mass flow to volume flow via .
and mean
temperature in kelvin and its rise across the cooling jacket.
and mean
specific heats at constant pressure and constant volume; always .
gives
the heat rate (watts) absorbed by the hydrogen in the walls.
is
enthalpy of an ideal gas, the turbine-extractable energy per kilogram.
and "ideal gas" mean
the gas constant in , with ; an approximation for real H₂.
is
(~1.4), the knob linking pressure ratio to temperature ratio.
The isentropic link is
.
is
— pump power demanded.
is
— turbine power supplied.
The self-sustaining condition is
.