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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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288 Musudan<br />

<strong>to</strong>gether. Two <strong>of</strong> the components served as boosters for<br />

the third stage, which was orbital. <strong>The</strong>se boosters could<br />

then be flown back either by pilots or by remote control.<br />

Fuel could be pumped from the boosters in<strong>to</strong> the orbiter,<br />

so the orbiter could reach orbit with a full fuel load and<br />

therefore, if required, continue on <strong>to</strong> the Moon.<br />

Musudan<br />

Launch site at 40.5° N, 129.5° E, from which North<br />

Korea attempted <strong>to</strong> launch its first satellite, Kwangmyongsong<br />

1, in 1998.<br />

MX-324<br />

An experimental American rocket-powered aircraft <strong>of</strong><br />

World War II built by Northrop Corporation with an<br />

Aerojet engine. <strong>The</strong> MX-324 had a length <strong>of</strong> 4.3 m, a<br />

wingspan <strong>of</strong> 11.6 m, a <strong>to</strong>p speed <strong>of</strong> 885 km/hr, and a<br />

maximum range <strong>of</strong> 1,600 km. Its maiden flight was on<br />

July 5, 1944, at Harper Dry Lake, California. <strong>The</strong> test<br />

pilot, Harry Crosby, lay prone in order <strong>to</strong> withstand the<br />

high acceleration. Only three <strong>of</strong> the planes were ever<br />

built: two were severely damaged during testing, and a<br />

third was dismantled.<br />

Myojo<br />

A NASDA (National Space Development Agency, <strong>of</strong><br />

Japan) payload attached <strong>to</strong> the H-2 launch vehicle <strong>to</strong><br />

moni<strong>to</strong>r the rocket’s performance, confirm the accuracy<br />

<strong>of</strong> the H-2 orbit injection, and collect data on the environment<br />

<strong>of</strong> the payload equipment; “Myojo” means<br />

“Venus.” It was also known as the Vehicle Evaluation Payload<br />

(VEP).<br />

Launch<br />

Date: February 3, 1994<br />

Vehicle: H-2<br />

Site: Tanegashima<br />

Orbit: 449 × 36,261 km × 28.6°<br />

Total mass: 2,391 kg

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