I answer 13 and it was within 10% of the right answer A spacecraft is in empty space. It carries on board a gyroscope with a moment of inertia of I, = 21.5 kg - m2 about the axisof the gyroscope. The moment of inertia of the spacecraft around the same axis is I, = 5.00 x 105 kg m2. Neither thespacecraft nor the gyroscope is originally rotating. The gyroscope can be powered up in a negligible period of time to anangular speed of 140 rad/s. If the orientation of the spacecraft is to be changed by 21.0°, for what time interval should thegyroscope be operated?131Your response differs from the correct answer by more than 100%. sAdditional MaterialsD eBook he Motion of Gyro Xer-11-problem-1142p-physics-for-scientists-and-engineers-technology-update-no-access-codes-included-9th-edition/9781305116399/section-115-the-motion-of-gyroscopesQ Search for textbooks, step-by-step explanations to homework questions,...E Ask aPhysics for Scientis... / Section 11.5 The Motion of Gyroscopes and Tops A spacecraft is in empty space. It carries on board gyroscope with a mo1.5 The Motion of Gyroscopes and Tops A spacecraft is in empty spaces for Scientists andChapter 11, Problem 11.42P口ee...onTextbook ProblemStuck on youad A. Serway +1 otherer: Cengage Learning781305116399Ask a question and ganswer in as fasSection 11.5 The Motion of Gyroscopes and TopsAsk anA spacecraft is in empty space. It carries on board gyroscope with29 of 30 quea moment of inertia of I, = 20.0 kg-m2 about the axis of theuntil 3/gyroscope. The moment of inertia of the spacecraft around theentum*Response times vasame axis is I, = 5.00 X 10° kg-m². Neither the spacecraft nor thequestion complexitytime is 34 minutes ancgyroscope is originally rotating. The gyroscope can be powered upin a negligible period of time to an angular speed of 100 rad/s. Ifthe orientation of the spacecraft is to be changed by 30.0°, fornew subonswhat time interval should the gyroscope be operated?Expert SolutionTo determineF4FSF6F7FBF9F10F12PAUS

Given data: Moment of inertia of spacecraft IS=5.00×105 kg·m2. Moment of inertia of gyroscope…

A spacecraft is in empty space. It carries on board a gyroscope with a moment of inertia of I, = 21.5 kg m2 about the axis of the gyroscope. The moment of inertia of the spacecraft around the same axis is 1̟ = 5.00 x 105 kg m². Neither the spacecraft nor the gyroscope is originally rotating. The gyroscope can be powered up in a negligible period of time to an angular speed of 140 rad/s. If the orientation of the spacecraft is to be changed by 21.0°, for what time interval should the gyroscope be operated?

A spacecraft is in empty space. It carries on board a gyroscope with a moment of inertia of I, = 21.5 kg m2 about the axis of the gyroscope. The moment of inertia of the spacecraft around the same axis is 1̟ = 5.00 x 105 kg m². Neither the spacecraft nor the gyroscope is originally rotating. The gyroscope can be powered up in a negligible period of time to an angular speed of 140 rad/s. If the orientation of the spacecraft is to be changed by 21.0°, for what time interval should the gyroscope be operated?