IOAA 2021, Теория — Задача 3. Mars (10 points).

Theory — Q3-1 English (Official) — Mars (10 points). · 10 т.

Standard Table of Constants — values used in this problem

Universal gravitational constant: G=6.674×10−11 N m2 kg−2G=6.674\times10^{-11}\ \mathrm{N\,m^2\,kg^{-2}}.

Standard Table of Constants — values used in this problem

Mars: mean radius 3 390 km3\ 390\ km; mass 6.417×1023 kg6.417\times10^{23}\ kg.

Условие

A spacecraft of mass m=5.0×104 kgm=5.0\times10^{4}\ \mathrm{kg} approaches in a parabolic orbit ABAB, with respect to Mars. When the spacecraft reaches point BB of least distance to the center of Mars, rB=6.8×106 mr_B = 6.8\times10^{6}\ \mathrm{m}, it undergoes an instantaneous deceleration using its rockets and goes into a perfectly calculated orbit so that it will touch the Martian surface exactly at point CC, diametrically opposite BB, as shown in the figure.

Mars and the spacecraft trajectory: incoming path AB, point B at distance r_B from the centre, and surface point C on the opposite side.

3.1 Determine the speed (km s−1)(km\ s^{-1}) of the spacecraft at point BB just before the deceleration. [3 т.]

3.2 Calculate the total energy (J)(J) of the spacecraft as it is moving between points B and C. [4 т.]

3.3 Calculate the speed (km s−1)(km\ s^{-1}) of the spacecraft at point CC. [3 т.]

Отговори

Решение

Внимание: Непълно решение

Official TQ3.pdf ends after 3.2 Solution A. The promised second method and all of 3.3 are absent; combined Theory Solutions.pdf page 3 has the same ending, with TQ4 starting on page 4.


Оригинал в Архива: TQ-3-Q.pdf · официални решения: TQ3.pdf · допълнителни данни: TQ-3-A.pdf · допълнителни данни: Standard-Table-of-constants.docx.pdf · допълнителни данни: TQ-G.pdf · допълнителни данни: data.pdf