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Apollo LLRV
Part of Apollo LM
Apollo LLRV
Apollo LLRV
Credit: NASA
American manned lunar lander test vehicle. Bell Aerosystems initially built two manned lunar landing research vehicles (LLRV) for NASA to assess the handling characteristics of Apollo LM-type vehicles on earth.

AKA: Apollo LLTV;Lunar Lander Test Vehicle;Lunar Landing Research Vehicle. Status: Operational 1965.

A follow-on contract for three 'production' versions for astronaut training were referred to as LLTV 'lunar landing training vehicles'.

The LLRV could take off and land under its own power, reaching an altitude of about 1,220 meters, hover, and fly horizontally. A fan turbojet engine provided a constant upward push of five-sixths the weight of the vehicle to simulate the one-sixth gravity of the lunar surface.

The LLRV's, humorously referred to as "flying bedsteads," were created by a predecessor of NASA's Dryden Flight Research Center to study and analyze piloting techniques needed to fly and land the tiny Apollo Lunar Module in the moon's airless environment. (Dryden was known as NASA's Flight Research Center from 1959 to 1976.)

Success of the LLRV's led to the building of three Lunar Landing Training Vehicles (LLTV's) used by Apollo astronauts at the Manned Spacecraft Center, Houston, TX, predecessor of NASA's Johnson Space Center.

Apollo 11 astronaut, Neil Armstrong first human to step onto the moon's surface said the mission would not have been successful without the type of simulation that resulted from the LLRV's and LLTV's.

Background

When Apollo planning was underway in 1960, NASA was looking for a simulator to profile the descent to the moon's surface. Three concepts were developed: an electronic simulator, a tethered device, and the ambitious Flight Research Center (FRC) contribution, a free-flying vehicle. All three became serious projects, but eventually the FRC's LLRV became the most significant one. Hubert Drake was credited with originating the idea, while Donald Bellman and Gene Matranga were senior engineers on the project, with Bellman the project manager.

After conceptual planning and meetings with engineers from Bell Aerosystems, Buffalo, NY, a company with experience in vertical takeoff and landing (VTOL) aircraft, NASA issued Bell a $50,000 study contract in December 1961. Bell had independently conceived a similar, free-flying simulator, and out of this study came the NASA Headquarters' endorsement of the LLRV concept, resulting in a $3.6 million production contract awarded to Bell Feb. 1, 1963, for delivery of the first of two vehicles for flight studies at the FRC within 14 months.

Built of aluminum alloy trusses and shaped like a giant four-legged bedstead, the vehicle was to simulate a lunar landing profile. To do this, the LLRV had a General Electric CF-700-2V turbofan engine mounted vertically in a gimbal, with 4200 lb of thrust. The engine got the vehicle up to the test altitude and was then throttled back to support five-sixths of the vehicle's weight, simulating the reduced gravity of the moon. Two hydrogen peroxide lift rockets with thrust that could be varied from 100 to 500 lb handled the LLRV's rate of descent and horizontal movement. Sixteen smaller hydrogen peroxide rockets, mounted in pairs, gave the pilot control in pitch, yaw, and roll. As safety backups on the LLRV, six 500-lb rockets could take over the lift function and stabilize the craft for a moment if the main jet engine failed. The pilot had a zero-zero ejection seat that would then lift him away to safety.

Flight Operations

The two LLRV's were shipped from Bell to the FRC in Apr. 1964, with program emphasis on vehicle No. 1. It was first readied for captured flight on a tilt table constructed at the FRC to test the engines without actually flying. The scene then shifted to the old South Base area of Edwards. On the day of the first flight, Oct. 30, 1964, research pilot Joe Walker flew it three times for a total of just under 60 seconds to a peak altitude of ten ft (3 m). Later flights were shared between Walker; another Center pilot, Don Mallick; the Army's Jack Kleuver; and NASA Manned Spacecraft Center, Houston, pilots Joseph Algranti and H.E. "Bud" Ream.

NASA had accumulated enough data from the LLRV flight program at the FRC by mid-1966 to give Bell a contract to deliver three LLTV's at a cost of $2.5 million each.

In Dec. 1966 vehicle No. 1 was shipped to Houston, followed by No. 2 in Jan. 1967, within weeks of its first flight. Modifications already made to No. 2 had given the pilot a three-axis side control stick and a more restrictive cockpit view, both features of the real Lunar Module that would later be flown by the astronauts down to the moon's surface.

When the LLRV's arrived at Houston, where research pilots would learn how to become LLTV instructor pilots, No. 2 had been flown just 7 times while No. 1, the veteran, had a total of 198 flights. In Dec. 1967, the first of the LLTV's joined the FRC's LLRV's to eventually make up the five-vehicle training and simulator fleet.

Three of the five vehicles were later destroyed in crashes at Houston - LLRV No. 1 in May 1968 and two LLTV's, in Dec. 1968 and Jan. 1971.

The two accidents in 1968, before the first lunar landing, did not deter Apollo program managers who enthusiastically relied on the vehicles for simulation and training.

Donald "Deke" Slayton, then NASA's astronaut chief, said there was no other way to simulate a moon landing except by flying the LLTV.

LLRV No. 2 was eventually returned to Dryden, where it was on display as a silent artifact of the Center's contribution to the Apollo program.



Family: Lunar lander test vehicle, Moon. Country: USA. Agency: Bell. Bibliography: 16, 2443, 2479, 2480, 2481, 2482, 2483, 2486, 376, 4436, 459.
Photo Gallery

Apollo LLRV 2 ViewApollo LLRV 2 View
Credit: NASA



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