Martin Marietta X-23

The Martin X-23A PRIME (Precision Reentry Including Maneuvering reEntry) (SV-5D) was a small lifting-body re-entry vehicle tested by the United States Air Force in the mid-1960s. Unlike ASSET, primarily used for structural and heating research, the X-23A PRIME was developed to study the effects of maneuvering during re-entry of Earth's atmosphere, including cross-range maneuvers up to from the ballistic track.

Design

Each X-23A was constructed from titanium, beryllium, stainless steel, and aluminium. The craft consisted of two sections—the aft main structure and a removable forward "glove section". The structure was completely covered with a Martin-developed ablative heat shield thick, and the Nose cone, nose cap was constructed of Pyrolytic carbon, carbon Phenol formaldehyde resin, phenolic material.

Aerodynamic control was provided by a pair of lower Flap (aircraft), flaps, and fixed upper flaps and Rudder#Aircraft rudders, rudders. A nitrogen-gas reaction control system was used outside the atmosphere. At Mach number, Mach 2 a drogue ballute deployed and slowed the vehicle's descent. As it deployed, its cable sliced the upper structure of the main equipment bay, allowing a recovery Parachute, chute to deploy. It would then be Mid-air retrieval, recovered in midair by a specially-equipped Lockheed C-130 Hercules, JC-130B Hercules aircraft.

Flight testing

The first PRIME vehicle was launched from Vandenberg AFB on 21 December 1966 atop an Atlas SLV-3 launch vehicle. This mission simulated a low Earth orbit reentry with a zero cross-range. The ballute deployed at , though the recovery parachute failed to completely deploy. The vehicle crashed into the Pacific Ocean.

The second vehicle was launched on 5 March 1967. This flight simulated a 654-mile (1053-kilometre) cross-range reentry, and banking at hypersonic speeds. The recovery parachute deployed properly and was located by two of the deployed recovery aircraft. During an inspection fly-by of the descending parachute system it was seen that reefing cutters had failed to actuate. These cutters are on the harness suspending the vehicle from the parachute to ensure stability of the vehicle behind the JC-130B recovery aircraft during reel-in, and permit safely boarding the vehicle. As a result, the parachute and vehicle were allowed to descend to the sea. Subsequently, the vehicle separated from its flotation "balloon" in the rough seas and, with the parachute, sank before a nearby ship could arrive to retrieve it from the ocean.

The final PRIME mission was flown on 19 April 1967, and simulated re-entry from low Earth orbit with a cross-range. This time, all systems performed perfectly, and the X-23A was successfully recovered. An inspection by a USAF-Martin team reported the craft "ready to fly again", although no later missions were carried out. The third X-23A is now on display at the National Museum of the United States Air Force at Wright-Patterson Air Force Base in Ohio.

Specifications (X-23A)

See also

References

External links

Encyclopedia AstronauticaVideo
Atlas X-38 Prototype Arrival (PRIME/X-23), Unloading, Mating and Launch

{{DEFAULTSORT:Martin X-23 Prime
United States military gliders
Lifting bodies
Spaceplanes
1960s United States experimental aircraft
Unmanned aerial vehicles of the United States
Martin aircraft, X-23
Aircraft first flown in 1966