3/29/2024 0 Comments Xf-84h![]() The XF-84H was the first aircraft to carry a retractable/extendable ram air turbine in the event of failure of the engine, it would automatically swing out into the airstream to provide hydraulic and electrical power. The tail was modified to a T-tail to avoid turbulent airflow flow over the horizontal stabilizer/elevator surfaces from propeller wash. Thrust was adjusted by changing the blade pitch. The 12 ft diameter Aeroproducts propeller consisted of three steel, square-tipped blades turning at a constant 3,000 rpm, with the tips travelling at approximately Mach 1.18. An afterburner was installed though never used, which could increase power to 7,230 hp (5,391 kW). The engine was changed to an Allison XT-40-A-1, capable of 5,850 hp (4,362 kW). The XF-84H was created by modifying a F-84F Thunderstreak aircraft. Navy requirement for a carrier fighter not requiring catapult assistance, although the USAF Wright Air Development Center was the key sponsor of the project. The initial inception for the program came from a U.S. ![]() Originally designated XF-106, the project and its resultant prototype aircraft were renamed XF-84H, suggesting it was a mere F-84 variant, rather than an entirely new type. ![]()
0 Comments
Leave a Reply. |
AuthorWrite something about yourself. No need to be fancy, just an overview. ArchivesCategories |