Bell Selected for Phase 1A of DARPA Speed and Runway Independent Technologies (SPRINT) X-Plane Program
Bell to leverage HSVTOL technology to inform Phase 1A conceptual design
news.bellflight.com
I think CSAR is going to be limited to V-22s and V-280s for a long time.The fan in wing drastically improves the flexibility to the logisticians and operational commanders with its fixed wing range, speed, with the flexibility of landing sites too. It does not however solve the CSAR/Medical Evacuation and to a lesser extent a set of the Special Operations missions.
The issue, I believe that while the fan in wing will likely not have the downwash velocities of a Harrier or F-35, I believe it would have greater down wash velocities than some of the missions called for. Higher than the current M/CV-22B. The Ospreys down wash velocity is already considered at the edge of viability for safe operations away from prepared surfaces. Certainly, the ability to land at much lower speeds on unimproved surfaces compared to a C-130 for instance, is a significant enhancement. However, mission sets that require prolonged VTOL, such as fast rope or foliage penetrator for CSAR seem very high risk. VTOL landing to small unimproved restrictive landing areas likewise would seem exceedingly high risk. This is more pronounce in those terrains where the bearing ratio of the land is that of a plowed field or less. While VTOL aircraft can overcome this challenge by maintaining hover and not putting the full weight on the landing gear, anything much higher velocity than the Osprey will likely begin to sling dirt and rocks in doing this. If I recall correctly there was a bit of Harrier lore from BAOR days about them "digging their own grave" on unimproved terrain and that the RAF had very effective engineers who could quickly establish "semi-improved" landing sites. While this might be a viable methodology still, I suspect that the ubiquitous ISR of our information age makes this higher risk. Roads and car parks in the parts of the world most likely to see this sort of operation tend to be high traffic volume areas, further exacerbating the observation challenge.
The ability of the fan in wing platform to move significant (C-130 sized loads[?]) over larger distances and perform VSTOL to roads and car parks is a drastic improvement over current runway dependent aircraft. I certainly hope to see the successful development of this concept for those reasons. I just do not see it fulfilling all of the mission sets that I have seen put forward for this HSVTOL program.
The RAF liked to lay pressed steel plates to “improve”’short-term forward operating bases for Harriers.….. If I recall correctly there was a bit of Harrier lore from BAOR days about them "digging their own grave" on unimproved terrain and that the RAF had very effective engineers who could quickly establish "semi-improved" landing sites. ….
A bit sad Ptero didn't get in on this.DARPA's Naval VTOL X-Plane Drone Program Narrows Down To Two Designs
Northrop Grumman and Sikorsky have been chosen to further develop designs for long-endurance naval VTOL drones.www.twz.com
View: https://x.com/DARPA/status/1793646045987066342
They did bid. They just didn't win, which was disappointing considering they look so cool.A bit sad Ptero didn't get in on this.
Interesting... Apparently they have already conducted flight demonstrations with its X-P4 prototype (39 kg) from the flight deck of the USNS Burlington during the U.S. Naval Forces Southern Command/U.S. 4th Fleet Hybrid Fleet Campaign Event (HFCE).They did bid. They just didn't win, which was disappointing considering they look so cool.
Sea state is calm, wind is fair but the offset in landing is over a meter. I doubt that this is quite a positive result.
(targeting point is defined by the QR code).
The team is currently designing an uncrewed demonstrator with a 45-ft wingspan and 1,000-pound payload capacity for the SPRINT program. The propulsion system includes off-the-shelf turbofan and turboshaft engines that would power the vehicle to a maximum of 450 knots true airspeed (KTAS).
The technology demonstrated in the SPRINT X-plane could be scaled to medium and heavy lift aircraft, creating a future family of systems. For example, Aurora envisions a manned, 130-ft wingspan aircraft with four lift fans and 40-ft payload bay. The FIW aircraft could meet or exceed the payloads, ranges, and speeds typical of fixed wing military transport aircraft while delivering the tactical advantage of true vertical takeoff and landing.
If it demonstrates payload/range/speed superior to a typical fixed-wing military transport, a CTOL derivative might be a possibility. On the other hand, the BWB airframe might not be big enough to take advantage of increased payload provided by removal of the lift systems and CTOL operations. The impracticality of stretching a BWB airframe is one of the configuration's downsides.A Revolutionary Solution for Contested Air Transport - Aurora Flight Sciences
Fan-in-wing technology powers Aurora’s concept for unprecedented speed and stealth in a vertical lift platform.www.aurora.aero
I could be wrong, but in this case, I am not sure that this propulsion methodology is going to land in fields any more than an F-35 or Harrier. It is still of significant benefit to be able to operate away from airfields.