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

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366 Schirra, Walter (“Wally”) Marty, Jr.<br />

on the first/second stage adapter ring were fired for<br />

4 seconds. As well as maintaining the positive motion<br />

<strong>of</strong> the rocket, this forced the second-stage fuel <strong>to</strong> the<br />

bot<strong>to</strong>m <strong>of</strong> its tanks in order <strong>to</strong> feed the engines—a socalled<br />

ullage maneuver—and was the cue for the five J-<br />

2 second-stage engines <strong>to</strong> ignite. Thirty seconds later,<br />

the first/second-stage adapter ring fell away, and six<br />

seconds after that, the escape <strong>to</strong>wer was jettisoned.<br />

<strong>The</strong> second-stage engines burned for 365 seconds<br />

before the next separation <strong>to</strong>ok place. Four solidfueled<br />

retro-rockets on the second stage fired <strong>to</strong> keep<br />

the second and third stages from colliding. <strong>The</strong>n the<br />

second stage began its drop in<strong>to</strong> the Atlantic about<br />

4,000 km from the launch site. At this point, the Saturn<br />

V was traveling about 25,300 km/hr at an altitude<br />

<strong>of</strong> 185 km. Two solid-fueled mo<strong>to</strong>rs on the third-stage<br />

aft skirt were fired briefly <strong>to</strong> settle the fuel, and, simultaneously,<br />

the S-IVB third-stage J-2 engine fired up for<br />

a burn <strong>of</strong> 142 seconds. This initial S-IVB burn carried<br />

<strong>Apollo</strong> in<strong>to</strong> a 190-km orbit at a speed <strong>of</strong> 28,200<br />

km/hr. During two or three checkout orbits, the S-IVB<br />

attitude control mo<strong>to</strong>rs could be fired in sequence <strong>to</strong><br />

make any necessary on-orbit corrections. Following<br />

these checkout orbits, the ullage mo<strong>to</strong>rs were fired for<br />

77 seconds <strong>to</strong> settle the fuel and provide forward<br />

spacecraft momentum. <strong>The</strong>n the third-stage J-2<br />

engine reignited for 345 seconds <strong>to</strong> achieve a speed <strong>of</strong><br />

40,000 km/hr and <strong>to</strong> place <strong>Apollo</strong> on a lunar trajec<strong>to</strong>ry.<br />

<strong>The</strong> third stage separated from the CSM/LM<br />

combination, and the third-stage ullage mo<strong>to</strong>rs fired<br />

for 280 seconds <strong>to</strong> move the S-IVB clear <strong>of</strong> <strong>Apollo</strong>.<br />

Finally, the J-2 fired for the last time, using up its<br />

remaining fuel and, depending on the mission pr<strong>of</strong>ile,<br />

sending the spent third stage <strong>to</strong>ward either deep space<br />

Schirra, Walter (“Wally”) Marty, Jr. (1935–)<br />

(continued from page 362)<br />

Flying an F3D night fighter, Schirra was the first <strong>to</strong> fire a<br />

Sidewinder at a drone target—with almost disastrous<br />

results. <strong>The</strong> missile went out <strong>of</strong> control and started <strong>to</strong><br />

loop around <strong>to</strong> chase the plane; Schirra’s response was <strong>to</strong><br />

make an even faster loop <strong>to</strong> stay on its tail. He flew the<br />

Mercury capsule Sigma 7 <strong>to</strong> become the third American<br />

in space, commanded Gemini 7, which made the first<br />

space rendezvous, and commanded <strong>Apollo</strong> 7. 262<br />

Schmidlap, Johann (sixteenth century)<br />

A German fireworks maker and perhaps the first, in 1591,<br />

<strong>to</strong> experiment with staging—a technique for lifting fire-<br />

or a collision with the Moon. <strong>The</strong>se intentional lunar<br />

impacts were <strong>to</strong> enable seismometers placed on the<br />

lunar surface by previous <strong>Apollo</strong> missions <strong>to</strong> detect<br />

the resulting “moonquakes” and <strong>to</strong> tell scientists<br />

about the Moon’s internal structure.<br />

Although a two-stage version <strong>of</strong> the Saturn V was<br />

used <strong>to</strong> place Skylab in orbit, the rocket was effectively<br />

retired at the end <strong>of</strong> the <strong>Apollo</strong> program. During<br />

its development, the Saturn V was expected <strong>to</strong><br />

become a workhorse booster <strong>of</strong> a planned <strong>Apollo</strong><br />

Applications space science program that would follow<br />

the lunar landing missions, but this program never<br />

materialized. In December 1976, NASA released components<br />

<strong>of</strong> two remaining vehicles along with test articles,<br />

which eventually enabled the completion <strong>of</strong><br />

three Saturn V displays.<br />

Overall length: 110.8 m (<strong>Apollo</strong>), 101.7 m (Skylab)<br />

Payload: 129,300 kg (LEO), 48,500 kg (Moon)<br />

First stage (S-IC)<br />

Size: 42 m (length); 10 m (diameter); 19.2 m<br />

(fin-span)<br />

Propellants: RP-1 and LOX<br />

Total thrust: 33,360,000 N (<strong>Apollo</strong>); 34,300,000<br />

N (Skylab)<br />

Second stage (S-II)<br />

Size: 24.8 m (length); 10 m (diameter)<br />

Propellants: liquid hydrogen and LOX<br />

Total thrust: 5,170,000 N (<strong>Apollo</strong>); 5,000,000 N<br />

(Skylab)<br />

Third stage (S-IVB)<br />

Size: 17.9 m (length); 6.6 m (diameter)<br />

Thrust: 1,030,000 N<br />

works <strong>to</strong> higher altitudes. A large skyrocket (first stage)<br />

carried a smaller skyrocket (second stage). When the large<br />

rocket burned out, the smaller one continued <strong>to</strong> a higher<br />

altitude before showering the sky with glowing cinders.<br />

Although Schmidlap appears <strong>to</strong> have been the first <strong>to</strong> fly<br />

staged rockets, priority for the idea may go <strong>to</strong> Conrad<br />

Haas.<br />

Schmiedl, Friedrich (1902–1994)<br />

An Austrian civil engineer who, beginning in 1918, carried<br />

out numerous experiments with solid-fueled rockets.<br />

In February 1931, he began a postal service using remotecontrolled<br />

rockets that landed by parachute <strong>to</strong> carry mail<br />

between neighboring <strong>to</strong>wns, primarily Schöckel and

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