Aeroplane and Commercial Aviation News, 102. kötet1962 |
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12. oldal
... stage - length that can be achieved . Fortunately , the thrust required to meet the design cruising condition is by no means so complicated . To all intents and purposes , irrespective of stage - length , the cruising thrust needed is ...
... stage - length that can be achieved . Fortunately , the thrust required to meet the design cruising condition is by no means so complicated . To all intents and purposes , irrespective of stage - length , the cruising thrust needed is ...
16. oldal
... stages and is driven by the two - stage H.P. turbine . It has a compression ratio of 6.5 : 1 and discharges air to the combustion zone at pressures up to 240 p.s.i.a. and a maximum temperature of about 470 ° C. The combustion zone ...
... stages and is driven by the two - stage H.P. turbine . It has a compression ratio of 6.5 : 1 and discharges air to the combustion zone at pressures up to 240 p.s.i.a. and a maximum temperature of about 470 ° C. The combustion zone ...
25. oldal
... stage - 70 to 80 ft . high and 33 ft . in diameter - will form the first stage of a three - stage launch vehicle which will carry the three - man Apollo spacecraft on circumlunar missions . The advanced Saturn also is intended to be ...
... stage - 70 to 80 ft . high and 33 ft . in diameter - will form the first stage of a three - stage launch vehicle which will carry the three - man Apollo spacecraft on circumlunar missions . The advanced Saturn also is intended to be ...
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