Agreed, the paint really makes a difference. We've got the traditional level of battleship grey to go ontop of that too.
A big difference is the WR-21 has an intercooling and recupration* arrangement on the top, this increases the height of the turbine to be greater than a deck. I've attached a pic of the WR-21 and that hump in the back end (compared to the roughly cuboid shape of the MT30) comes from the Int/Rec gear being attached.
Here's a very good piece by Beedall about it, but it's more in a CVF context.
Early studies showed that four WR-21's in an IFEP configuration could propel a 30-40,000 tonnes CVF at a maximum speed of 30 knots. However as CVF grew in size, speed inevitably dropped. During 2002, with the BAE and Thales teams now considering CVF concepts of 60,000 tonnes or more, the new Rolls-Royce Marine Trent MT30 became increasingly favoured over the WR21. Because of it's significantly greater power output (36MW compared with 25MW), fewer GTA packages are required for achieving the required generating power.
Indeed despite being 45% more powerful than the WR21, the MT30 unit actually requires far less volume and weighs much less than the WR21 when the latter's complex intercooled and recuperating system is included. Also, although no figures are published, it is likely that the MT30 costs less to procure, although over a 20+ year life cycle the higher fuel efficiency of the WR21 starts to tell in terms of saving on fuel cost and overall through life costs
Navy Matters | CVF Propulsion
Considering the Type 26 needs to have a
cheap unit cost first and foremost, it's understandable why it was picked. Once you add in the fact it's got a greater power generating capacity but is lighter and smaller, it's not that bad of a package deal.
But i'd still like the idea of having a common GTA arrangement, we're definitely going to have a mixed pool and it's generally believed that the Type 26's will have the MT30 but who knows, could be the WR21.
*the intercooler and recuperation package greatly increases fuel efficiency, this is torn straight from RR
The intercooler, located between the compressor sections, cools the intermediate-pressure compressor (IPC) air before it enters the high-pressure compressor (HPC). This reduces the HPC inlet temperature and therefore HPC work to deliver a significant boost in engine power. The intercooler also enhances recuperator effectiveness, as the inlet temperature is reduced thereby increasing exhaust heat recovery.
The recuperator recovers and transfers heat energy from the hot exhaust, which is used to preheat combustion air, therefore much less fuel is required to reach the same power turbine entry temperature (PTET). As a result less fuel is used to achieve the same power. Recovering heat energy from the exhaust gas also reduces its temperature giving a reduced infrared (IR) signature.
WR-21 Marine gas turbine - Rolls-Royce
So the intercooler basically makes the recuperator more effective, and it's the recuperator that increases the fuel efficiency. So as is, if you slapped the same sort of packages onto the MT30 you'd get the same results as what you'd get for the WR-21 at a cost of an increased procurement cost (and weight/size) but lower through life cost. It might even have been worked out that the sort of performance benefits of doing such a thing aren't worth the financial investment of implementing it