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LUNAR LANDING RESEARCH VEHICLE
I joined the X-15 program as a civilian contractor for
NASA. The NASA High Range Tracking stations were located at Ely and
Beatty
Nevada with main control being at Dryden/Edwards AFB in California. I
was assigned to the tracking station at Beatty, Nevada as part of a
crew consisting of a Station Manager, a Technical Advisor, and field
engineers for the Mod-2 Radar, Data Transmission System,
Communications, Telemetry, and Plant Maintenance/Generators. NASA had a
site monitor at each tracking station to monitor our contractor
operations.
Though supporting flights of the X-15 was our main objective, we also
participated in flights of the XB-70, the Lifting Bodies, an occasional
A-12/SR-71 Blackbird flight, and the experimental Lunar Landing
vehicles depicted below.
The LLRVs, 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 LLRVs led to the building of three Lunar Landing
Training Vehicles (LLTVs) used by Apollo astronauts at the Manned
Spacecraft Center, Houston, Texas, 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 LLRVs and LLTVs.
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 is 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, N.Y., 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 on 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 4,200 pounds 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 pounds 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-pound 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
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 feet (3 m). Later flights were
shared between Walker; another Dryden pilot, Don Mallick; the Army's
Jack Kleuver; and NASA Manned Spacecraft Center 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 LLTVs at a
cost of $2.5 million each.
In December 1966 vehicle No. 1 was shipped to Houston, followed by No.
2 in January 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 LLRVs 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 December 1967,
the first of the LLTVs joined the FRC's LLRVs 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 LLTVs, in December 1968 and
January 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 is on display as
a silent artifact of the Center's contribution to the Apollo program.
The LLRV project linked above paved the way for the following:
In 1967 I spent a few months at the Flight Dynamics Laboratory at Wright Patterson AFB performing structure integrity tests on the Apollo 1 Space Capsule. The capsule below is one I recently visited at Astronaut and Air Force Lt. Gen. Thomas P. Stafford's museum in Weatherford, Oklahoma. Ironically, Gen. Stafford was one of the pilots of the Soviets MiGs while I was at Area 51 for Projects Have Drill and Have Doughnut. .
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