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Which of the following is/are the prime considerations in space vehicles and aircraft?(a) High strength-weight ratios for materials and high ratios of payload to the vehicle’s weight(b) High strength-weight ratios for materials only(c) High ratios of payload to vehicles weight only(d) Neither high strength-weight ratios for materials nor high ratios of payload to the vehicle’s weightI have been asked this question during a job interview.This intriguing question comes from Environments topic in chapter Other Environments of Corrosion Engineering |
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Answer» Right option is (a) HIGH strength-weight ratios for materials and high ratios of payload to the VEHICLE’s weight |
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