Title: ALV X-1
Content:  ALV X-1 was the first and only flight of the ATK Launch Vehicle (ALV) sounding rocket developed by Alliant Techsystems. The launch occurred from LP-0B at the Mid-Atlantic Regional Spaceport (MARS) at NASA's Wallops Flight Facility. This mission carried the SOAREX-VI and Hy-BoLT experiments as payloads when it launched at 09:10 GMT on August 22, 2008. The vehicle was terminated 20 seconds into flight after veering too far off course.
Title: ALV X-1
Content:  Sub-Orbital Aerodynamic Re-entry EXperiments VI (SOAREX-VI) was sponsored by the Hypersonics Project within the Fundamental Aeronautics Program of NASA, and developed by NASA's Ames Research Center. It was carried by the ALV X-1 as a secondary payload. SOAREX-VI would have attempted to characterize an innovative self-orienting reentry vehicle shape called the Slotted Compression RAMP (SCRAMP) probe. The SOAREX-VI package also included an atmospheric density calibration probe built by NASA Ames in cooperation with the University of Idaho, and an AIS probe built by the United States Naval Research Laboratory (NRL). After detonation of the rocket, the SOAREX-VI enclosure inside was broken open. The SCRAMP probe, designed to activate upon ejection, did exactly that and acquired two TDRSS satellites overhead and an S-band tracking dish on land. It transmitted sensor and video data until it was destroyed on splashdown.
Title: Temco XKDT Teal
Content:  The XKDT was designed for use an inexpensive and expendable air-launched, high-performance target drone. Its design utilized a low-set swept wing, and an inverted cruciform tail; the structure of the aircraft included aluminum honeycomb wing construction and extensive use of magnesium and fiberglass in the fuselage. It was intended to reach speeds of up to Mach 0.95. The Teal could be launched at any altitude of up to 50000 ft; speed at launch was between 163 kn and 248 kn. Following launch a dual-thrust solid fuel rocket motor ignited; thrust was 150 lbf for the first four seconds of powered flight, followed by 50 lbf for approximately 500 seconds propulsive time. Control was provided by a three-axis autopilot; radar reflectors and infrared flares provided an assist in tracking the drone, and at the end of nine minutes' flight time a self-destruct device would be activated.
Title: ALKA (weapon)
Content:  The ALKA directed-energy weapon (DEW) system is a Turkish dual electromagnetic/laser weapon developed by Roketsan. It was first unveiled at the 2019 IDEF exhibition on 8 May 2019. This combat laser was allegedly used to destroy one of GNC's Wing Loong II UAVs; if true, this would represent the first known time a vehicle mounted combat laser was used to destroy another combat vehicle during genuine wartime conditions.
Title: ACMAT ALTV
Content:  ALTV means Acmat Light Tactical Vehicle. It is a derivative of the Nissan Navara. It has a payload of 1.4 to 3.5 tonnes, depending on the version. The ALTV is marketed under several variants, such as station wagon, single cab, double cab or torpedo.
Title: Aerola Alatus
Content: AL-12 ; Initial unpowered prototype ; AL-12M ; Initial powered prototype ; Alatus ; Production model pure glider with an empty weight of 80 kg and a gross weight of 200 kg. Conforms to German LTF and LFG requirements. ; Alatus-M ; Production model motor glider with an empty weight of 115 kg and a gross weight of 235 kg. Conforms to German LTF and LFG requirements, as well as US FAR 103 Ultralight Vehicles rules. Powered by a pylon-mounted retractable 20 hp CorsAir M25Y ES engine that produces a climb rate of 2.0 m/s (400 fpm) and gives an endurance of 1.5 hours. An electric powerplant is also available which provides a half-hour endurance. The Alatus-M can be converted back to the Alatus by removing the powerplant pylon and engine. 
Title: ALKA (weapon)
Content:  The ALKA DEW is claimed to have a power of 50 kW. It operates both laser and electromagnetic systems. It purportedly uses ATR while using both electro-optical and radar detection to track multiple targets simultaneously. It is claimed by its designers to have the capability to disable a swarm of drones at a range of 4000 m, destroy a target with laser at 500 m distance and destroy a target at 1000 m distance with electromagnetic weapons. According to the designers, it can track targets at speeds as high as 150 km/h and track targets with precision of 8 mm at 1000 m distance. It can purportedly operate in both night and day time and on multiple platforms, both stationary and mobile. It has allegedly been used both against IEDs and UAVs in multiple environments.
Title: Moyes XT
Content:  The XT is an intermediate-level hang glider made from aluminum tubing, with the mostly single-surface wing covered in Dacron sailcloth. It was marketed as easy to fly, possessing a low stall speed and responsive handling. The aircraft was produced in two sizes named after its wing area in square feet, to accommodate pilots of different weight ranges.
Title: North American X-10
Content:   To facilitate development of the long-range Navaho surface-to-surface cruise missile, North American Aviation (NAA) developed the RTV-A-5 (Research Test Vehicle, Air Force), or X-10 in 1951. This vehicle was to prove critical flight technology for the design of the Navaho cruise missile. These included proving the basic aerodynamics to Mach 2, flight testing the inertial guidance unit and flight control avionics to the same speed, and validate the recovery system for the next phase in the Navaho program. Preliminary design of the X-10 was completed in February 1951 and the first vehicle was delivered to Edwards Air Force Base in May 1953. The first flight occurred on 14 October 1953. The X-10 was powered by two Westinghouse J40 
Title: Scout X-1
Content:  Scout X-1 was an American expendable launch system and sounding rocket which was flown seven times between August 1960 and October 1961. Four orbital and three suborbital launches were made, with four of the launches resulting in failures. The Scout X-1 was similar to the Scout X test vehicle which was launched in April 1960, however it had live second and fourth stages, as opposed to the battleship versions used on the Scout X. It also featured an improved first stage, using an Algol 1B instead of the earlier Algol 1A used on the Scout X. All seven launches occurred from Launch Area 3 at the Wallops Flight Facility. The maiden flight was a suborbital 

Question: Verify the following claims with "True" or "False": They make both the ALV X-1 and the XM25 CDTE.
Answer: True