The Complete Book of Spaceflight: From Apollo 1 to Zero Gravity
The Complete Book of Spaceflight: From Apollo 1 to Zero Gravity
The Complete Book of Spaceflight: From Apollo 1 to Zero Gravity
Create successful ePaper yourself
Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.
368 Schweikart, Russell (“Rusty”) L.<br />
Corps Reserve in 1933 after completing pilot training. He<br />
earned an M.A. in aeronautical engineering from Stanford<br />
in 1942 and then flew 63 combat missions in the<br />
Pacific <strong>The</strong>ater during World War II. In 1954, he became<br />
commander <strong>of</strong> the Western Development Division (soon<br />
renamed the Air Force Ballistic Missile Division) and<br />
from 1959 <strong>to</strong> 1966 was commander <strong>of</strong> its parent organization,<br />
the Air Research and Development Command<br />
(renamed Air Force Systems Command in 1961). As<br />
such, he oversaw the development <strong>of</strong> the Atlas, Thor,<br />
and Titan missiles, introducing a systems approach<br />
whereby the various components <strong>of</strong> the Atlas and succeeding<br />
missiles underwent simultaneous design and testing.<br />
Schriever also instigated the practice <strong>of</strong> concurrency,<br />
which allowed the components <strong>of</strong> missiles <strong>to</strong> enter production<br />
while still in the test phase, thereby speeding up<br />
development. He retired as a general in 1966. 215<br />
Schweikart, Russell (“Rusty”) L. (1935–)<br />
An American astronaut who served as the Lunar Module<br />
(LM) pilot on <strong>Apollo</strong> 9, the mission during which<br />
the LM was tested for the first time in space. Schweikart<br />
attended the Massachusetts Institute <strong>of</strong> Technology<br />
(MIT), earning a B.S. in aeronautical engineering and<br />
an M.S. in aeronautics and astronautics. Following graduation,<br />
he served as a pilot in the U.S. Air Force and Air<br />
National Guard (1956–1963). During part <strong>of</strong> this period<br />
he worked as a research scientist in the Experimental<br />
Astronomy Labora<strong>to</strong>ry at MIT. Schweikart joined<br />
NASA in Oc<strong>to</strong>ber 1963 as one <strong>of</strong> 14 selected in the<br />
third group <strong>of</strong> astronauts. Later he moved <strong>to</strong> NASA<br />
Headquarters in Washing<strong>to</strong>n as direc<strong>to</strong>r <strong>of</strong> user affairs<br />
in the Office <strong>of</strong> Applications, responsible for transferring<br />
NASA technology <strong>to</strong> the outside world. He then<br />
held several technology-related positions with the California<br />
state government, including assistant <strong>to</strong> the governor<br />
for science and technology and, in 1979, as<br />
chairman <strong>of</strong> the California Energy Commission.<br />
Schweikart is currently president <strong>of</strong> Aloha Networks.<br />
SCORE (Signal Corps Orbiting Relay Experiment)<br />
An American satellite, nicknamed “Chatterbox,” that<br />
relayed the first voice communications from space. Its<br />
payload included an audio tape machine that broadcast<br />
messages, including a 58-word prerecorded Christmas<br />
message from President Eisenhower, for 13 days.<br />
Launch<br />
Date: December 18, 1958<br />
Vehicle: Atlas B<br />
Site: Cape Canaveral<br />
Orbit: 185 × 1,484 km × 32.3°<br />
Mass: 70 kg<br />
Scott, David R. (1932–)<br />
An American astronaut who was the pilot on Gemini 8,<br />
Command Module pilot on <strong>Apollo</strong> 9, and commander<br />
<strong>of</strong> <strong>Apollo</strong> 15. Scott received a B.S. from the U.S. Military<br />
Academy in 1954 and an M.S. in aeronautics and astronautics<br />
from the Massachusetts Institute <strong>of</strong> Technology<br />
in 1962. He entered the Air Force and graduated from the<br />
Experimental Test Pilot School and Aerospace Research<br />
Pilot School at Edwards Air Force Base before being<br />
selected by NASA as an astronaut in 1963. Later, he held<br />
administrative posts with NASA, including direc<strong>to</strong>r <strong>of</strong><br />
the Dryden Flight Research Center. Scott retired from the<br />
Air Force in 1975 as a colonel and is currently president<br />
<strong>of</strong> Scott Science and Technology. 265<br />
Scout<br />
A small rocket, 21.9 m high and 1 m in diameter, able <strong>to</strong><br />
launch lightweight satellites or perform high-altitude<br />
research at relatively low cost. Conceived by NACA<br />
(National Advisory Committee on Aeronautics) in 1958,<br />
the Scout program was taken over by the Langley<br />
Research Center when NASA was created in Oc<strong>to</strong>ber<br />
1958. In less than a year, Scout emerged as a four-stage<br />
vehicle that could serve as a sounding rocket or small<br />
satellite launcher. NASA decided that all four stages<br />
would be solid-fueled, citing the relative simplicity and<br />
reliability <strong>of</strong> previously demonstrated solid-fuel technology.<br />
<strong>The</strong> Scout first stage, called Algor, was adapted from<br />
the Polaris missile program. Controlled by the moveable<br />
outer tips <strong>of</strong> four stabilizer fins in conjunction with four<br />
exhaust deflec<strong>to</strong>r vanes, it burned for 40 seconds and<br />
could produce a thrust <strong>of</strong> 510,000 new<strong>to</strong>ns (N). <strong>The</strong> second<br />
stage also had its roots in a military program. Called<br />
Cas<strong>to</strong>r, it originated with the Army Sergeant rocket program.<br />
It burned for 39 seconds, was stabilized by hydrogen<br />
peroxide jets, and could produce a thrust <strong>of</strong> 225,000<br />
N. <strong>The</strong> third stage, Antares, was an upgraded version <strong>of</strong><br />
the Vanguard Altair third stage. It burned for 39 seconds,<br />
was stabilized by hydrogen peroxide jets, and could produce<br />
61,000 N <strong>of</strong> thrust. An actual Vanguard Altair third<br />
stage was incorporated as the Scout’s fourth stage. This<br />
burned for 38 seconds, was spin-stabilized, and could<br />
produce a thrust <strong>of</strong> 13,700 N. Both the third and fourth<br />
stages were encased in a glass-fiber shield that included<br />
the payload shroud and a device <strong>to</strong> spin-stabilize the<br />
fourth stage. <strong>The</strong> Scout was able <strong>to</strong> carry a 23-kg payload<br />
on a ballistic trajec<strong>to</strong>ry <strong>to</strong> an altitude <strong>of</strong> 13,700 km or a<br />
68-kg payload in<strong>to</strong> low Earth orbit. <strong>The</strong> original NASA<br />
Scout was modified for Air Force applications under the<br />
designations Blue Scout I, Blue Scout II, and Blue Scout<br />
Junior. In addition, a single Blue Scout II rocket was<br />
modified by NASA for use in the Mercury program and<br />
became known as the Mercury-Scout.