Title: Luna 3
Content:  The space probe was a cylindric canister with hemispheric ends and a wide flange near the top. The probe was 130 cm long and 12 cm at its maximum diameter at the flange. Most of the cylindric section was roughly 95 cm in diameter. The canister was hermetically sealed and pressurized to about 0.22 atm. Several solar cells were mounted on the outside of the cylinder, and these provided electric power to the storage batteries inside the space probe. Shutters for thermal control were positioned along the cylinder and opened to expose a radiating surface when the internal temperature exceeded 25 C. The upper hemisphere of the probe held the covered opening for the cameras. Four antennas protruded from the top of the probe and two from its bottom. 
Title: Luna 3
Content:  After launching on a Luna 8K72 (number I1-8) rocket over the North Pole, the Blok-E escape stage was shut down by radio control to put Luna 3 on its course to the Moon. Initial radio contact showed that the signal from the space probe was only about one-half as strong as expected, and the internal temperature was rising. The spacecraft spin axis was reoriented and some equipment was shut down, resulting in a temperature drop from 40 °C to about 30 °C. At a distance of 60,000 to 70,000 km from the Moon, the orientation system was turned on and the spacecraft rotation was stopped. The lower end of the craft was pointed at 
Title: Luna E-3 No.1
Content:  Luna E-3 No.1, sometimes identified by NASA as Luna 1960A, was a Soviet spacecraft which was lost in a launch failure in 1960. It was a 279 kg Luna E-3 spacecraft, the first of two to be launched, both of which were lost in launch failures. It was intended to fly around the Moon on a circumlunar trajectory in order to image the surface of the Moon, including the far side. The E-3 spacecraft were similar in design to the E-2A which had been used for the earlier Luna 3 mission. However, they carried higher resolution cameras, and were intended to make closer flybys.
Title: Luna E-3 No.2
Content:  Luna E-3 No.2, sometimes identified by NASA as Luna 1960B, was a Soviet spacecraft which was lost in a launch failure in 1960. It was a 279 kg Luna E-3 spacecraft, the second of two to be launched, both of which were lost in launch failures. It was intended to fly around the moon on a circumlunar trajectory in order to image the surface of the Moon, including the far side. The E-3 spacecraft were similar in design to the E-2A which had been used for the earlier Luna 3 mission. However, they carried higher-resolution cameras, and were intended to make closer flybys.
Title: Luna 9
Content:  Luna 9 was launched by a Molniya-M rocket, serial number 103-32, flying from Site 31/6 at the Baikonur Cosmodrome in the Kazakh Soviet Socialist Republic. Liftoff took place at 11:41:37 GMT on 31 January 1966. The first three stages of the four-stage carrier rocket injected the payload and fourth stage into low Earth orbit, at an altitude of 168 by and an inclination of 51.8°. The fourth stage, a Blok-L, then fired to raise the perigee of the orbit to a new apogee approximately 500000 km, before deploying Luna 9 into a highly elliptical geocentric orbit. For thermal control, the spacecraft then spun itself up to 0.67 rpm using nitrogen jets. On 1 February at 19:29 GMT, a mid-course correction took place involving a 48-second burn and resulting in a delta-v of 71.2 m/s.
Title: Luna 20
Content:  surface. A second firing further reduced velocity before Luna 20 set down safely on the Moon at 19:19 UT on 21 February 1972 at coordinates 3.7863 North and 56.6242 East, only 1.8 kilometers from the crash site of Luna 18. After collecting a small sample of lunar soil, the spacecraft's ascent stage lifted off at 22:58 UT on 22 February and quickly accelerated to 2.7 kilometers per second velocity—sufficient to return to Earth. The small spherical capsule eventually parachuted down safely on an island in the Karkingir River, 40 kilometers north of the town of Jezkazgan in Kazakhstan, at 19:19 UT on 25 February 1972. The 55-gram soil sample differed 
Title: Luna 23
Content:  62° east longitude. During landing in "unfavorable" terrain, the lander's drilling device was evidently damaged, preventing fulfillment of the primary mission, the return of lunar soil to Earth. Scientists devised a makeshift plan to conduct a limited science exploration program with the stationary lander. Controllers maintained contact with the spacecraft until 9 November 1974. High resolution orbital photographs taken by the NASA Lunar Reconnaissance Orbiter and released in March 2012 showed the Luna 23 spacecraft lying on its side on the lunar surface. The spacecraft evidently tipped over upon landing, perhaps due to higher than nominal vertical and/or horizontal velocities at touchdown.
Title: Luna E-3 No.2
Content:  Luna E-3 No.2 was launched at 16:07:41 UTC on 16 April 1960, atop a Luna 8K72 carrier rocket, flying from Site 1/5 at the Baikonur Cosmodrome. The Blok-B strap-on booster reached only 75% thrust and broke away from the booster almost immediately at liftoff. The launch vehicle climbed to an altitude of about 200 meters before the imbalanced thrust caused it to pitch over, the remaining strap-ons breaking off and scattering in random directions. Two of them plummeted to the ground while the third flew over the head of terrified spectators before impacting and exploding near the vehicle assembly building, shattering its windows. The core stage continued flying for some distance until crashing into a salt lake about two kilometers from the pad. Considerable damage to launch facilities resulted from this mishap. Prior to the release of information about its mission, NASA correctly identified that it had been an attempted circumlunar imagery mission.
Title: Luna 13
Content:  being supplied by a minute explosive charge. The other boom carried a backscatter densitometer that was used to infer the density of the lunar near-surface regolith. Four radiometers recorded infrared radiation from the surface indicating a noon temperature of 117 ±3 °C while a radiation detector indicated that radiation levels would be less than hazardous for humans. The lander returned a total of five panoramas of the lunar surface, showing a more smooth terrain than seen by Luna 9. One of the two cameras (intended to return stereo images) failed, but this did not diminish the quality of the photographs. The penetrometer measured the regolith density at 800Kg/m3. After a fully successful mission, contact was lost at 06:13 UTC on 28 December when the on-board batteries were exhausted.
Title: Luna E-3 No.1
Content:  Luna E-3 No.1 was launched at 15:06:45 UTC on 15 April 1960, atop a Luna 8K72 carrier rocket, flying from Site 1/5 at the Baikonur Cosmodrome. The core stage and strap-ons of the 8K72 booster performed perfectly and Blok E staging and engine start went well at first, but about halfway through its burn, engine thrust and fuel system pressure began dropping, followed by cutoff. Velocity was about 300 feet per second too low to escape the Earth's gravity, and the Blok E and probe fell back into the atmosphere and burned up. The cause of the failure was unclear until further examination of telemetry data found that the RP-1 tank in the Blok E stage was only partially filled, a careless mistake by pad crews that caused the booster to literally and figuratively run out of gas before it could escape Earth orbit. As a result, the spacecraft failed to achieve orbit. Prior to the release of information about its mission, NASA correctly identified that it had been an attempted circumlunar imagery mission.

Question: Verify the following claims with "True" or "False": The A-Rosa Luna is only 321200.0 millimetres long.
Answer: False