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The Complete Book of Spaceflight: From Apollo 1 to Zero Gravity

The Complete Book of Spaceflight: From Apollo 1 to Zero Gravity

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316 parking orbit<br />

rifled barrel with a 6-m-long smoothbore extension. After<br />

65 shells had been fired, each <strong>of</strong> progressively larger caliber<br />

<strong>to</strong> allow for wear, the barrel was rebored <strong>to</strong> a caliber<br />

<strong>of</strong> 240-mm. <strong>The</strong> German goal <strong>of</strong> their great cannon was<br />

not <strong>to</strong> destroy the French capital—it was far <strong>to</strong>o inaccurate<br />

a device for that (although it killed 256)—but <strong>to</strong> erode<br />

the morale <strong>of</strong> the Parisians. A similar giant gun with the<br />

same objective, the V-3, was built during World War II.<br />

Technologically, the Paris Gun can be seen as the first<br />

serious attempt <strong>to</strong> build a launch system with the capability<br />

<strong>of</strong> a space cannon.<br />

parking orbit<br />

An intermediate, waiting orbit adopted by a spacecraft<br />

between two phases <strong>of</strong> a mission.<br />

Parus<br />

A network <strong>of</strong> military satellites that, for a quarter <strong>of</strong> a<br />

century, has provided navigational information and<br />

s<strong>to</strong>re-dump radio communications for Russian/Soviet<br />

naval forces and ballistic missile submarines. Being the<br />

operational successor <strong>to</strong> Tsyklon, Parus is also known as<br />

Tsyklon-B. Flight trials <strong>of</strong> the new satellites began in<br />

1974, and the system was accepted in<strong>to</strong> military service in<br />

1976. <strong>From</strong> 1974 <strong>to</strong> the present, there have been about 90<br />

launches in the series, all by Cosmos-3M rockets from<br />

Plesetsk, in<strong>to</strong> roughly circular orbits with an altitude <strong>of</strong><br />

about 1,000 km and an inclination <strong>of</strong> 83°.<br />

passive satellite<br />

A satellite that simply reflects light or radio waves transmitted<br />

from one ground terminal <strong>to</strong> another without<br />

amplification or retransmission. An example is the Echo<br />

series <strong>of</strong> orbiting balloons.<br />

Pathfinder<br />

See Mars Pathfinder.<br />

Patrick Air Force Base<br />

A U.S. Air Force base located at the south end <strong>of</strong> Cape<br />

Canaveral, 19 km southeast <strong>of</strong> Cocoa, which is home <strong>to</strong><br />

the 45th Space Wing <strong>of</strong> the Air Force Space Command.<br />

Patrick AFB operates the Cape Canaveral Air Force Station,<br />

from which many military and nonmilitary launches<br />

take place. <strong>The</strong> base is named after Major General Mason<br />

M. Patrick, chief <strong>of</strong> the Army Air Service (1921–1926) and<br />

chief <strong>of</strong> the Army Air Corps (1926–1927), and was established<br />

following the transfer <strong>of</strong> control <strong>of</strong> the Banana<br />

River Air Station, set up in 1940 <strong>to</strong> support Atlantic coastline<br />

defense, from the Navy <strong>to</strong> the Air Force.<br />

Paulet, Pedro E.<br />

A Peruvian chemical engineer reputed <strong>to</strong> have conducted<br />

experiments in Paris, beginning in 1895, on a rocket<br />

engine made <strong>of</strong> vanadium steel that burned a combination<br />

<strong>of</strong> nitrogen peroxide and gasoline. If true, this<br />

would credit Paulet as the designer <strong>of</strong> the first liquidfueled<br />

rocket. <strong>The</strong> engine was described as weighing<br />

about 5 lb and using spark gap ignition <strong>of</strong> the fuels<br />

within a combustion chamber. It was said <strong>to</strong> have been<br />

capable <strong>of</strong> producing a 200-lb thrust at 300 sparks per<br />

minute. Paulet claimed that his rocket engine could burn<br />

continuously for as much as one hour without suffering<br />

any ill effects. However, news <strong>of</strong> what may have been a<br />

groundbreaking advance in rocketry did not surface until<br />

Oc<strong>to</strong>ber 27, 1927, when a letter from Paulet appeared in<br />

an issue <strong>of</strong> the Peruvian publication El Comercio, in<br />

which he claimed legal ownership <strong>of</strong> his earlier rocket<br />

engine design. Recognizing that rocketry was beginning<br />

<strong>to</strong> boom in Europe, Paulet sought witnesses <strong>to</strong> help verify<br />

the work he said he had done years earlier. <strong>The</strong> letter<br />

was circulated across the world by a Russian named<br />

Alexander Scherschevsky in summary form. Had Paulet’s<br />

work been authenticated, he would <strong>to</strong>day be considered<br />

the undisputed father <strong>of</strong> liquid propellant rocketry. As it<br />

is, that title is more commonly attributed <strong>to</strong> Robert<br />

Goddard.<br />

PAW ascent<br />

“Powered all the way” ascent: one that follows the shortest<br />

distance between Earth and a point in Earth orbit.<br />

PAW ascents consume the most fuel and are not considered<br />

feasible for orbits higher than 230 km.<br />

payload<br />

<strong>The</strong> load carried by an aircraft or rocket over and above<br />

what is necessary for the operation <strong>of</strong> the vehicle during<br />

its flight.<br />

Payload Assist Module (PAM)<br />

A solid mo<strong>to</strong>r developed for the Space Shuttle program.<br />

Its purpose is <strong>to</strong> lift a satellite from the parking orbit in<strong>to</strong><br />

which it is placed by the Shuttle <strong>to</strong> a higher, designated<br />

orbit from which the spacecraft will actually operate. A<br />

special PAM, known as PAM-D, was adapted for use with<br />

Delta launch vehicles.<br />

payload integration<br />

<strong>The</strong> process <strong>of</strong> bringing <strong>to</strong>gether individual experiments,<br />

support equipment, and s<strong>of</strong>tware in<strong>to</strong> a single payload in<br />

which all interfaces are compatible and whose operation<br />

has been fully checked out.<br />

payload ratio<br />

<strong>The</strong> ratio <strong>of</strong> the mass <strong>of</strong> useful payload <strong>of</strong> a rocketpropelled<br />

vehicle <strong>to</strong> the <strong>to</strong>tal launch mass <strong>of</strong> the vehicle.<br />

See rocket equation.

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