For the role of lobbing air launched long range hypersonic munitions from thousands of km away, why even use a manned or LO platform at all? Why not design an unmanned platform that is essentially a jet powered reusable booster with loitering capability?
It's dictated by the size of the payload, the range needed to get to the launch point, and the survivability of the platform.
- Payload size: a large weapon will need a large employment aircraft to house and carry it and get it into the air.
- Range to launch point: even assuming your payload has a relatively long range (let's say 2000km for the sake of argument), if your target is 8000km away, then your employment aircraft needs to be able to travel 6000km before it can launch the payload
- Survivability: your aircraft needs to be able to travel those 6000km in a manner where it is not intercepted, and ideally not detected so that the enemy doesn't have early warning to optimize/prepare their defenses against your payload.
Based on all of that, you inevitably will end up with a relatively large aircraft that has to be quite stealthy. We'll get to whether it is manned or unmanned later below in this post.
An aircraft which is not LO/VLO in nature is simply not useful even if it can physically accommodate the payload and has the range to the launch point, it will lack survivability against enemy early warning radars and CAP.
Putting it another way -- just because your employment aircraft doesn't have to do overhead bombing missions against an IADS, does not mean LO/VLO is not still vital. For the PLA, even if they are able to achieve air superiority over the western pacific, if they are wanting to conduct strikes against targets at Hawaii distances or Australia distances or even west coast of US distances, then part of their mission profile is going to be flying in more contested airspace even if it's over the open ocean rather than directly into the teeth of enemy IADS.
.... once the above prerequisites are all met, then it becomes a simple question of:
A) Do you want your employment aircraft to be a one way platform?
My Answer: a one way platform in theory could be cheaper and smaller as it doesn't have to return to home, but considering the above prior three prerequisites you still end up with a large and expensive aircraft so tossing those away as one way/single use platforms seems like a waste, meaning it should likely be a regular multi-use aircraft.
B) Do you want your employment aircraft to be manned or unmanned?
My Answer: considering all of the above characteristics, you're going to have a rather large, stealthy, capable aircraft, so putting in a cockpit for manned control of such a high value asset seems prudent. Furthermore, a manned crew in the aircraft also means you can use the aircraft for a variety of other mission profiles including being an airborne command/control asset, as well as ISR and EW. Which isn't to say that the aircraft cannot be designed to be "optionally manned" for certain specific mission profiles if needed. But it does mean that it should likely have a cockpit as a baseline feature.
Given all that, I don't really see a realistic way in which such an aircraft could not be a large, stealthy, manned bomber... which to be honest is not too different to what we always envisioned for H-20 to begin with anyhow.
The only difference now is that weapons bay length seems to be a driving design feature, which means a regular long wingspan flying wing won't work for it.
H-20 should have no problem carrying munitions with 2000-3000km range even without an oversized IWB. If we are talking about a platform for carrying even larger missiles, then such a missile would be expected to have ranges of 5000-8000km, at which point we are no longer talking about a tactical system.
Carrying 2000-3000km range subsonic weapons is absolutely doable by a flying wing H-20 (B-2 esque geometry and size aircraft).
But, if you're wanting 2000-3000km range hypersonic weapons, especially weapons with a relevant/useful sized warhead and onboard ECM and ECCM, then that is a whole different matter.
Well, I sure am interested to see how H-20 will turn out. Massive 10-15m long bays for the aforementioned air-launched HCM while also maintaining best in class stealth while also having global reach. I expect it to be different from the B-2/B-21 because there is no way a B-2/B-21 can fit both a long and massive bay while having wingspan under an acceptable length, doubt it'll be cranked arrow/beaked as studies show it is much less stealthy.
To be honest, a modified, but enlarged planform that is like J-36 or X-47A in geometry could be somewhat viable for the aircraft we are thinking. And it could be only subsonic; adopting such a planform doesn't mean it will need to be supersonic capable at all.