On 4 January 1955 the USAF issued Systems Requirement SR-12 for the Weapons System WS-118P high-speed reconnaissance vehicle.
Range was to be over 5000 km, altitude over 30 km. Bell provided a proposal on 1 December 1955, calling for a three-phase program using a glider designed to be boosted by a two-stage rocket to Mach 15 at 50 km altitude (Phase I would produce an 8,000 km range vehicle; Phase II a 16,000 km range vehicle; and Phase III an orbital vehicle).
Below are some of the documents released on this program.
Aircraft Configuration Survey for Weapon System 118P [62 Pages, 2.33mb]
Phase 3 Preliminary Development Plan [12 Pages, 1.17mb]
Reconnaissance System 118P Phase 3 [114 Pages, 5.29mb]
Standard Aircraft Characteristics, Phase 2 1/2, Weapon System 118P HIGH-ALTITUDE RECONNAISSANCE [20 Pages, 701k]