The Partnership: A History of the Apollo-Soyuz Test Project
Chapter 10
Final Examinations
[285] In May 1975, George
Low traveled once again to the Soviet Union, this time to inspect the
Soviet spacecraft and to jointly chair the Flight Readiness Review
(ERR). As with the Mid-Term Review, Low's correspondence prior to the
meeting had been with Soviet Academy President Keldysh. When the NASA
delegation arrived in Moscow, Petrov told Low that Keldysh's health
had taken another turn for the worse; he was in the hospital. Three
days later Petrov gave Low the news - Keldysh had decided to step
down from his post. Vladimir Aleksandrovich Kotelnikov, as acting
President, would supervise the FRR for the Soviet side. Kotelnikov,
who had a good command of English, at 63 was well known throughout
the U.S.S.R. for his textbooks in the field of radio and electronics
engineering. While saddened at the news of Keldysh's poor health, Low
knew he could work with his successor. But prior to the review, Low
and his colleagues visited Baykonur.
Final checkout of the American communications
equipment and the docking target alignment tests had been carried out
at the Baykonur Cosmodrome during mid-May. This last major activity
involved 16 Americans and their Soviet colleagues under the direction
of R. H. Dietz and B. V. Nikitin. They had finished their work on the
17th, ahead of schedule, in time for Low; Arnold Frutkin; Glynn
Lunney; John F. Yardley, the Associate Administrator for Manned Space
Flight; and Walter J. Kapryan, the Director of Launch Operations at
Kennedy Space Center (KSC), to visit the cosmodrome on an inspection
and orientation tour. Low and his group left Moscow's Vnukovo airport
on the afternoon of the 18th. After an evening's stay at the
Cosmonauts' Hotel in Leninsk, the five Americans and Professor
Bushuyev set out for the launch pad in the van usually reserved for
transporting the cosmonauts. Their ride took them through the launch
site industrial area to the launch stand.
At the launch pad, they stopped first at a
small monument commemorating Sputnik
I, which had been launched from this
stand on 4 October 1957. Low noted in his trip report:
[This same] pad was used for
Sputnik I, for Gagarin's flight, and will be used for one of the ASTP
birds. We asked how many launch vehicles had gone off
[286] this pad and got two different answers: one being 100
and the second being 300. It was well preserved and painted, and
apparently had been repainted prior to our visit. The basic
sequencing is all mechanical. The vehicle is not held down but is
guided by various arms which are part of the stand. It flies out of
the launch pad without holddown, and the arms and booms which support
the launch vehicle fall back under counter balance and the force of
gravity. Various platforms underneath the launch vehicle are moveable
and apparently collapse in a certain way so that they can all be
rolled underneath the pad.1
Low also reported that it was very windy at
Baykonur. He had been told "that the temperatures in the summertime
go to 40°C and in the winter to -40°C," The Soviets
indicated that a minimum of work was done out of doors in the winter
months.
While at the launch stand, the Soviets and
Americans discussed various aspects of launching spacecraft. Bushuyev
and Dmitri Bolshakov, the director of the Baykonur Cosmodrome, were
interested to learn why the U.S. launch vehicles were held down for a
short period of time after the engines were ignited. The Americans
explained that this ensured smooth combustion and thrust buildup.
Only after the engines were running satisfactorily were the launch
vehicles released. Low noted, "apparently [the Soviets] measure the
thrust buildup curve for all 20 engines and can shut down during the
buildup until just before lift-off." Since they did not need a hold
down system, they avoided this complex procedure. The Soviet launch
vehicle was also "slightly more efficient . . . from the point of
view of fuel consumption," and the Soviets said that they had never
lost a launch vehicle as a result of improper thrust
buildup.2
From the launch pad, the Americans were taken to the industrial area
where the spacecraft were readied for their flights.
Since the industrial sector was only a short
distance from the pad and since there were homes and a hotel there,
Low asked if this area was evacuated during launches. Bolshakov
responded that it was cleared just before a flight. After the
Americans were escorted into a huge building that housed the
equipment used to check out spacecraft systems, they visited the
Soviet equivalent of the KSC vehicle assembly building. Along one
side of the building, the prime launch vehicle rested horizontally.
The two spacecraft (prime and backup), which the astronauts had
examined in April and which Dietz' team had checked out earlier that
month, were also housed here. Low recorded that he "spent
considerable time walking around the launch vehicle"; he "asked a lot
of questions all of which were answered." He had been told earlier
that "the same [kind of] launch vehicle had been used since October
1957 and the first Sputnik launch." Low concluded that the Soviets
periodically introduced "block changes" into the launch vehicles
[287] either to enhance reliability or to replace
obsolescent component parts. He continued his report:
We were told that the ASTP launch
vehicle is one in a series of which more than 10 have already been
flown. The April 5 launch was conducted with a launch vehicle left
over from the previous series. The failure of the April 5 launch was
explained to us again in detail, and our people appear to be
satisfied with the explanation and with the fact that the changes
made in the ASTP launch vehicle should prevent this kind of failure.
The launch vehicle (all three stages) was on the right hand side of
the center aisle. On the left side were the two spacecraft and the
spacecraft shrouds. The launch vehicle was horizontal; the spacecraft
were vertical. In order to place the spacecraft inside the shrouds,
they are tipped to a horizontal position and cantilevered
horizontally from the launch stand. The shroud is then slid over the
spacecraft and attached to the bottom ring. At some point in the
process, the spacecraft is then taken out on a railroad car and
fueled. Then the launch vehicle and spacecraft are mated in a
horizontal position on the car which ultimately takes them to the
launch pad.3
The Americans spent the remainder of their
visit to Baykonur attending a briefing on the communications
electromagnetic compatibility tests just...
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Above, George Low (right)
visits the Soviet monument commemorating the launching of
Sputnik
I in October
1957. Others present are, left to right, W. J. Kapryan, G.
S. Lunney, and A. W. Frutkin. Inside the
Manned Spacecraft Assembly Building at Baykonur, George Low
(center), Professor Bushuyev, and the Soviet interpreter
listen to a briefing on the Soyuz launch vehicle. The
first-stage engine nozzles are visible at the far
fight. Both ASTP Soyuz spacecraft are being readied
for the joint mission. The extended solar panels will be
folded back so that the protective launch shroud (white
cylinder to the left of the far craft) can enclose the
spacecraft (Soviet Academy of Sciences photo).
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[288] ...completed,
touring the Korolev and Gagarin cottages at the launch site, and
visiting Leninsk. During the stop at the Korolev house, the Americans
got a rare insight into Bushuyev's past. Throughout ASTP, the Soviets
had given the Americans little information about their personal
backgrounds in the space program. But when the U.S. team visited
Korolev's cottage, "Bushuyev told us that he spent much time there
with Korolev and apparently stayed there on several occasions," Low
noted. On further questioning, Bushuyev told them that he had started
working with Korolev right after World War II on the launch vehicle
for Sputnik and on the spacecraft, too. Since then, he said, he had
concentrated mostly on spacecraft. The Americans and their Soviet
hosts then returned to Moscow for the FRR.4
1. George M. Low, "Notes
from Visit to Soviet Union, May 17-23, 1975," 5 June 1975.
2. Ibid.
3. Ibid.
4. Ibid.
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