You are trying too hard to look at TVM as a form of SARH, whereas it is really a type of command guidance. The distances of the target and missile are known to the ground radar, because it tracks them both. The same for their speed. At minimum, the reflection picked up by the missile seeker is used to refine the angular resolution of the target. I can easily thinks of ways the missile could get range and speed data, but that may not even be necessary as both are known to the ground radar.
Isn't that essentially how ICWI works? Even some old radars like the AWG-9 could provide PD illumination for SARH missiles like the Sparrow or even guide the Phoenix in SARH. I think they called that the PD STT (pulse doppler single target track) mode. Actually, the AIM-7F was the last Sparrow to support both CW and PD homing. All subsequent variants supported PD mode only (ICWI). So you see, PD "illumination" is possible in multi-static configuration.
A bit more info, from the Radar Handbook by Skolnik, on how PD illumination SARH works, and why it is desirable. Also, how it compares to ARH.
Its called Track Via Missile for something and the reason why TVM exists in the first place is because Command Guidance alone can be inaccurate for terminal homing. While the distances of the target and the missile can be known by the ground radar, unfortunately there is still a variance and error, and the farther it goes, the greater it gets. That's one reason why CG is literally gone from longer ranged SAMs and still exists in some very close ranged SAMs like a Tor or a Croatale. The whole point of TVM is that the ground radar is not trusted for its data, and whether you want to refine existing data or to not trust the ground station data, its still a bistatic application. Let me remind you that the reason why you have variance and error with speed measurement in the first place is that what you would expect for medium to low PRF from the ground station against a target over long range. The higher the PRF the more accurate it gets; when you reach infinite PRF, its literally Continuous Wave.
Going back to the SPG-51. The fact that you have a monopulse CWI means the CWI can track the target on its own. In other words the C-band PD doesn't need to operate to track for the monopulse CWI which can track a target on its own (minus range information). As a matter of fact, simultaneous PC and CWI operation on the same antenna imposes quite some interference when you have both circuits in transmit and receive. The reason for having a separate PD and CWI feed is more likely because one is a C-band feed and the other is an X-band feed. The horns for each has to be sized and separated appropriately by the physical wavelength and can't be used for one or the other. If the PD and CW are both X-band, they can time share between the same feed.
P STT or PD STT For AWG 9 (F-14 radar for you folks) is PD to support actively guided Phoenix missile. If you are using Sparrows on SARH with P STT or PD STT, its really on CW and not PD. The label is retained for convenience.
As for Skolnik, the Brimstone and the RBS-15 are already real world examples that he is wrong. These are actively guided missiles that use FMCW while sharing single antenna for both transmit and receive.
ICW does not solve the isolation problem completely unfortunately and neither does high PRF PD. If the range of the reflected object exceeds the time allotted by the receive period of the current duty cycle, the echoes will fall on the next duty cycle and on the next. As such, the antenna can receive these echoes while the antenna is transmitting on the next succeeding cycles. These echoes will be regarded as ambiguous data or ambiguous range.