significantly hampered by the post-war exodus of engineering talent. Shortly after the new definition was produced, this project also moved to the RAE. Efforts by the Navy to change the name from Seaslug to the more ominous-sounding "Triumph" failed. Development slowed, and in July 1947 the Admiralty approached Henry Tizard to argue for a more "virile leadership" of the program. Tizard called a meeting of the Defence Research Policy Committee (DRPC) and started a process of pushing through four key missile programs that were intended to enter service in 1957, Seaslug, a corresponding Army/Air Force missile known as Red Heathen, the Blue Boar television guided glide bomb, and the Red Hawk air-to-air missile. In March 1948 a new report from the DRPC noted there was not enough manpower for all four projects, and put Seaslug at the bottom of the priority list, claiming air attack would be less likely than submarine in the event of war. They suggested the much longer ranged Red Heathen was more important in the short term. The Admiralty was of another opinion on the matter and argued against the change in priority. The Navy found an unlikely ally in the Army, who were concerned that Red Heathen was too difficult to move to in a single stage and suggested that Seaslug might be the basis for a more immediate medium-range weapon that could be used both on land and sea. The DPRC also began to have concerns about guiding Red Heathen at its maximum range. In September 1948 they agreed to develop Seaslug "as a matter of insurance", before further upgrading it in 1949 to "top priority". As a result of these changes, the program was seen as having two stages, Stage 1 would deliver missiles in the mid-1950s with roughly range with capability mostly against subsonic targets, and a Stage 2 of the early 1960s would have a greatly extended range on the order of and able to attack supersonic aircraft. Experimental systems Two test systems emerged from this centralization. The CTV.1 was a small unpowered Brakemine-like system devoted to the development of the guidance systems, launched using three RP-3 rocket motors and controlled through the coast phase. A series of CTV designs followed, providing ever-increasing amounts of telemetry for the guidance and control systems work. GAP became a purely research-oriented system, RTV.1 (rocket test vehicle), as opposed to a prototype missile design, and