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Which of the following is a disadvantage of N 2 O4 /MMH propellant? I. It is highly toxic. II. It delivers imprecise delta-V, generally requiring
Which of the following is a disadvantage of N 2 O4 /MMH propellant? I. It is highly toxic. II. It delivers imprecise delta-V, generally requiring long thrust times. III. The oxidizer (N2 O4 ) requires far larger tanks than the fuel (MMH), introducing design complexity and increasing parts count. IV. It offers higher Isp than cold-gas propulsion
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