Title: Luna (yacht)
Content: 10 VIP guest cabins over 100 square metres each, a 20-metre outdoor swimming pool, 9 decks, a large outdoor entertaining area, 8 tenders, 1 mini-submarine, and a crew of 50 persons ; An anti-missile system like Eclipse, bulletproof windows to VR9+ levels, a steel hull over 17.5 cm thick, LRAD guns, bomb-resistant doors, FLIR, and an anti-drone system ; 2 helipads rated over 7.5 tons capacity, which host Akhmedov's Eurocopter EC155 B1 and EC145 (registered M-LVNA and M-LUNA) simultaneously ; 4 stabilizers: 2 quantum-stabilizers and 2 fin-stabilizers ; 7 diesel-electric generators, providing a total output of over 15,000 hp ; 1 stern thruster jet providing dynamic positioning within accuracy of 20 cm ; 1 million liter fuel tank (over 1,000 tons), enabling a cruise of over 9,000 nm at economical speeds of 16-18 knots Luna and Eclipse have the only multipurpose custom made lifeboat-limousines in the world at a cost of over $4m each. They are capable of acting as VIP transport and being lifeboats at the same time. Other features include:
Title: Luna E-8 No.201
Content:  Luna E-8 No.201, also known as Luna Ye-8 No.201, and sometimes identified by NASA as Luna 1969A, was a Soviet spacecraft which was lost in a launch failure in 1969. It was a 5590 kg Luna E-8 spacecraft, the first of three to be launched, It was intended to perform a soft landing on the Moon, in order to deploy a Lunokhod rover onto the surface. It carried the Lunokhod No.201 rover.
Title: Luna 24
Content:  Luna 24 was based on the Ye-8-5 spacecraft body, consisting of two attached stages, an ascent stage mounted on top of a descent stage. The lander stood 3.96 meters tall and had an unfueled landed mass of 1880 kg. With a full load of fuel its launch mass was between 5600 and 5750 kg. The descent stage was the same as the Ye-8 lower stage for the Lunokhod rovers, a cylindrical body with four protruding landing legs, fuel tanks, a landing radar altimeter, and a dual descent engine complex. The main descent rocket, the KTDU-417, was a throttleable 1920 kg thrust engine used for mid-course corrections, orbit insertion, braking for descent to the surface, and to 
Title: Euroluna
Content:  , EuroLuna was designing a lightweight solar-powered four-wheeled Luna Rover called ROMIT, which will be pared down to just 110 pounds by minimising redundant systems.
Title: Luna 24
Content:  spherical top which replaced the Lunokhod rover and housing from the Ye-8 bus. It carried a cylindrical hermetically sealed soil sample container inside a spherical re-entry capsule, mounted on a 1920 kg thrust KRD-61 rocket. Total mass of the ascent stage was 520 kg, of which 245 kg was the nitric acid and UDMH propellant. It was 2 meters tall. The sample return cabin was 50 cm in diameter and had a mass of 39 kg. The KRD-61 could only fire once, for 53 seconds, to put it on a free return trajectory to Earth. Specific impulse of the engine was 313 seconds, it could impart a velocity of 2600-2700 m/s to the return craft.
Title: 1862 Apollo
Content:  On November 4, 2005, it was announced that an asteroid moon, or satellite of Apollo, had been detected by radar observations from Arecibo Observatory, Puerto Rico, October 29 &ndash; November 2, 2005. The announcement is contained in the International Astronomical Union Circular (IAUC) 8627. The satellite is only 80 m across and orbits Apollo just 3 km away from the asteroid itself. From the surface of Apollo, S/2005 (1862) 1 would have an angular diameter of about 2.0835 degrees.
Title: Moon
Content:  (LRO) and the LCROSS impactor and follow-up observation orbiter on 18 June 2009; LCROSS completed its mission by making a planned and widely observed impact in the crater Cabeus on 9 October 2009, whereas LRO is currently in operation, obtaining precise lunar altimetry and high-resolution imagery. In November 2011, the LRO passed over the large and bright crater Aristarchus. NASA released photos of the crater on 25 December 2011. Two NASA GRAIL spacecraft began orbiting the Moon around 1 January 2012, on a mission to learn more about the Moon's internal structure. NASA's LADEE probe, designed to study the lunar exosphere, achieved orbit on 6 October 2013.
Title: Luna E-6 No.6
Content:  Luna E-6 No.6, sometimes identified by NASA as Luna 1964A, and sometimes known in the West as Sputnik 27, was a Soviet spacecraft which was lost in a launch failure in 1964. It was a 1422 kg Luna Ye-6 spacecraft, the fourth of twelve to be launched. It was intended to be the first spacecraft to perform a soft landing on the Moon, a goal which would eventually be accomplished by the final Ye-6 spacecraft, Luna 9. Luna E-6 No.6 was launched at 08:15:35 UTC on 21 March 1964, atop a Molniya-M 8K78M carrier rocket, flying from Site 1/5 at the Baikonur Cosmodrome. A connecting rod in the Blok I stage broke, leading to a propellant valve failing to open completely. The stage developed insufficient thrust to reach orbit and it shut down at T+489 seconds. The upper stages and probe reentered the atmosphere and broke up. Prior to the release of information about its mission, NASA correctly identified that it had been an attempt to land a spacecraft on the Moon.
Title: First Lunar Outpost
Content:  The landing vehicle was designed to be as simple and easy to operate as possible. It would weigh 93,526 kg (103 tons) and be powered by four RL-10 engines. When fully deployed its landing legs would stretch to a massive 18.8 meters wide and would stand 14.1 meters tall. Each FLO crewed flight would only require one launch and one vehicle. The Comet would send the lander on a trajectory to the lunar surface where it would then use its engines to brake and land. From the surface, the ascent vehicle would carry the crew capsule directly back to Earth. This was similar to the early Apollo direct ascent.
Title: Luna 24
Content:  Luna 24 was the third attempt to recover a sample from the unexplored Mare Crisium, the location of a large lunar mascon (after Luna 23 and a launch failure in October 1975). After a trajectory correction on 11 August 1976, Luna 24 entered lunar orbit three days later. Initial orbital parameters were 115 by at 120° inclination. After further changes to its orbit, Luna 24 set down safely on the lunar surface at 06:36 UTC on 18 August 1976 at 12°45' North latitude and 62°12' East longitude, not far from where Luna 23 had landed. Exact landing location (12.7145° N, 

Question: Verify the following claims with "True" or "False": The A-Rosa Luna, christened 4/7/2005, is 125800.0 millimetres long and weighs 1850 tons.
Answer: True