Part C ✪ 0 Review Constants around s orbit, it he high earth's Using conservation of energy, find the speed at perigee and the speed at apogee. Enter your answers in meters per second separated by a comma. h Uperigee, Vapogee = ΟΙ ΑΣΦ 7 0 ? m/s Submit Request Answer Part D It is necessary to have the spacecraft escape from the earth completely. If the spacecraft's rockets are fired at perigee, by how much would the speed have to be increased to achieve this? Express your answer in meters per second. 8 ( 9 K Auperigee = hp O L 110 114 O ■跖 Ο ΑΣΦ 12 ? m/s 2 11:46 PM 714 5/7/2024 ins prt sc delete home end { } P [ ] backspace num lock 7 home enter 4 TA 0. + PRE pg up pg dn 88 5 9 66 pg up 69 Δυραίκου = Ο ΑΣΦ Submit Request Answer Part E What if the rockets were fired at apogee? Express your answer in meters per second. ΜΕ ΑΣΦ Avapogee = Submit Request Answer < Return to Assignment Provide Feedback m/s m/s on Inc. All rights reserved. | Terms of Use | Privacy Policy | Permissions | Contact Us | 9 hp L 110 O C f12 ما O + 11:46 PM 5/7/2024 PRE ✈ ins prt sc delete home end pg up pg + 11 t backspace num lock