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Challenge 4

This challenge closed on 13/11/2019. See below for the correct answers.

A Narrow Escape

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Meg, I have been working through the list of suspicious incidents affecting Apollo Eleven and it is longer than you might think. The pre-launch, stage three thruster valve problem is a little suspicious given all the checks that took place before that, but on the other hand telemetry guaranteed that it would be detected and the technicians showed that it was easy to bypass. If that was a sabotage attempt then it wasn’t very well designed, so I don’t think it could have been an engineer that set it up. On the other hand, no-one else would have had time alone with the component. On the other hand, someone from FIDO’s team sent me a message to tell me about a very near miss that sounds like it could have been a serious attempt to destroy the command module on re-entry. As Apollo XI approached the re-entry point they jettisoned the Service Module to re-orient the Command Module so that the heatshield was pointing into the atmosphere. Since they were on pretty much a ballistic orbit the SM would have stayed close to the CM, and without a heatshield of its own it would break up into large pieces that posed a significant danger to the CM and its crew. To avoid that the SM was supposed to carry out a sequence of short burns to move its trajectory away from the Command Module, skipping it off the atmosphere so that the CM could re-enter free from the debris field. Unfortunately, that doesn’t seem to have happened. Aldrin reported that the CM flew past the SM which was flying at an attack angle well beyond operational parameters, and a commercial pilot, Frank Brown, reported seeing the two spacecraft tracking closely as they burned through the atmosphere. A single collision with one of the white-hot fragments could have badly damaged the re-entry capsule, and even if the astronauts had survived the collision then the odds are that the parachute system would have triggered early or been fatally damaged by the blast. NASA engineers are working fast to correct the problem for Apollo XIII and they have mitigations in place for XII’s re-entry, but the view of the experts is that they dodged a bullet with this. The flight officer who reported it to me pointed out that if the Soviets wanted to sabotage the mission this might have been a good bet: it was a nasty accident that was hard to foresee, and it will be very difficult to show that someone deliberately miscalculated the burn times since it was the interaction of the thrusters and stabilisers that caused the problem. I think he is one of a growing number of NASA employees who have begun to believe that the USSR has deep cover agents working to destabilise the programme. My worry is that even if he is wrong, the lack of trust that is growing within the organisation will destabilise it on its own. I am really hoping he is mistaken. The success of Apollo XI seems to have bought a lot of international goodwill and I think it could be the start of something more positive. The Soviet cooperation with the landing gave me hope that we could find more common ground and start to thaw East-West relations, but this could really threaten that. In the mean-time we had better step up security. I think we should use a simple Vigenere cipher with period two for our next message. I have encrypted the attached re-entry report using a columnar transposition cipher.

Separation anxiety

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Apollo XI Postflight Analysis Spacecraft Re-entry Trajectory Review This document contains information about the events during the re-entry phase of Apollo XI. It has been compiled to satisfy flight planning/safety requirements. The review covers the following mission phase: Trans Earth coast, which ends with re-entry into the mid-Pacific recovery area. The original flight plan called for separation of the CM from the SM twelve minutes before entry interface. Successful separation would then trigger a sequence of burns intended to stabilise the Service Module and to move it out of the re-entry corridor to avoid debris collisions with the Command Module during the re-entry phase. The reaction control system burn sequence involved both the roll and the Minus-X jets . The attitude burns were intended to set up a roll in order to stabilise remaining fuel and to prevent uncontrolled gyration during the boost. That would have then taken the SM out of the re-entry corridor into a high-altitude orbit that would decay only after the command module had landed. In the event the sequence of burns did not achieve the required trajectory shift, with reports from the astronauts on board and from a commercial airline pilot, that the two space vehicles re-entered the atmosphere together, with the CM passing the SM during the plasma burn phase. Given the proximity of the vehicles during re-entry it is considered highly fortunate that no debris from the relatively unprotected SM struck the CM, and simulations show that such a strike would have been likely to cause catastrophic damage to the CM. Possible defects arising from a collision include: i. Heatshield damage. Even a minor crack in one of the heatshield panels would be likely to cause superheating which could breach the hull leading to further catastrophic damage to the vehicle with probable loss of life. ii. Premature firing of the parachute pyrotechnics, leading to full or partial loss of the descent arrest system and loss of life. iii. Damage to the parachute shield might have prevented the pyrotechnics from releasing the parachutes leading to a catastrophic collision on landing and loss of life. iv. Damage to one or more of the parachutes could have led to a high velocity impact with probable resulting injuries and possible loss of life. The high likelihood of catastrophic failure arising from the deviation from flight parameters means that further analysis of the separation burn strategy is required. Pending that, remediation for the Apollo XII re-entry trajectory is a high priority. It is suggested that surplus fuel should be ejected from the SM before the separation burn begins in order to stabilise the attitude, and that the Minus-X burns should be timed to coincide with the roll jets to improve stability.