Approximately 30 minutes later at 106 hours we still expect the burst disc on the supercritical helium tank of the LM descent stage to go and vent that helium tank overboard. A-15. Remarkably, their unwieldy stack has reached a very stable attitude for the moment, and they are ready to start the PTC rotation. Product description A special new edition of the Apollo 13 Manual, published to coincide with the 50th Anniversary of the Moon mission launched in April 1970, which very … The targeting for the perigee after this burn 19.8 nautical miles versus present perigee of 87 nautical miles. The Suit Temp rheostat controls the temperature of the oxygen in the suit circuit by managing the flow of the coolant glycol into the regenerative heat exchanger. The increasingly uncomfortable crew of Apollo 13 has accomplished another important task on their unexpectedly early return home. The burst disc range is 1,881 to 1,970 per square inch. Fred is not wrong in his musings. We will wait until the burst disk on the super critical helium goes before we reestablishing passive thermal control, however. >> i would like to start by saying i am not a superstitious person. Please read this description: Apollo 13 - The Infamous Manual Burn This video covers the infamous manual burn with the LMs DPS engine. These somewhat disjointed comments are one side of a conversation between Jim and presumably Fred in the Lunar Module. NASA/NARA. Buy Apollo 13, 1970 (Including Saturn V, CM-109, SM-109, Lm7: An Insight Into the Development, Events and Legacy of NASA's 'Successful Failure' (Owners' Workshop Manual) on Amazon.com FREE SHIPPING on qualified orders The total duration of both the descent propulsion system and the trim burn was 15.4 seconds. Lot 6463 Flown double-sided checklist page carried on board Apollo 13, headed “LMA790-3-LM, Apollo Operations Handbook,” pages 11–12 from the “Apollo 13 Flight Data File,” 8 x 10.5, signed in black ballpoint, “James Lovell, Apollo 13 CDR.” MSC Apollo 13 Investigations Team - Final Report - Panel 6, Related Systems Evaluation - Volume II - Lunar Module. Although Earth viewed through the COAS will be the main visual reference, the crew is passed information on the AOT's use for this purpose as well. Lunar Module maneuver PADs do not have room for Earth entry information. We can only speculate what Jim was planning to do here upon returning home. Apollo 13 now 155,111 nautical miles from Earth. Flight Director, Milton Windler and the Maroon Team of Flight Controllers are replacing Flight Director, Gerry Griffin and the Gold Team. The target level during the power down is to keep it to at least 14 amps, so we're well below the minimum target, and in very good shape on LM power at this time. As Apollo 13 entered the Lunar corridor, the command service module (CSM) separated from the third stage and maneuvered around to extract the lunar module.That was the portion of the spacecraft that would take the astronauts to the Moon. This is Apollo Control at 105 hours, 37 minutes. They can add the extra 0.4 fps by firing the LM's downward-facing RCS thrusters (those that point in the same direction as the DPS) so that the total retrograde Delta-V is 7.8. It contains information about the Saturn V system, range safety and instrumentation, monitoring and control, prelaunch events, and pogo oscillations. . One of our large LM status boards here in Mission Control would indicate that the power down in the LM is completed at this time. They are 282,622 kilometers away from Earth and their velocity is 1,356.4 m/s. We can expect venting anytime up to and within the next 2 hours probably. 16mm film capture. Apollo EECOM , by Sy Liebergot with David M. Harland (Apogee Books, 2003). The Mission was on track. The latest prediction is that we'll reach the lower limit, the burst limit, the lower burst limit 1,881 at in about an hour and a half. Following this burn, passive thermal control will be reestablished, and the command module pilot, Jack Swigert, and the lunar module pilot, Fred Haise, will begin a 6 hour rest period. When word got out that Apollo 13 was in trouble, off-duty flight controllers and spacecraft systems experts began to gather at MSC, to be available if needed. by Alan Boyle on June 25, 2019 at 10:30 am July 27, 2019 at 8:56 pm. Had they been following the regular flight plan, their landing was scheduled for 103:42:02 GET, exactly two hours previously. We'll pass that along to you as soon as it is available. "Quality Control.Go Flight!" Apollo 11 flight manual expected to sell for millions at moon landing anniversary auction. The burn looked good. . They've picked up 40 m/s of velocity in the last two hours from the increasing pull of Earth's gravity. Photos in: Mike Pacak's Pinball Flyer Reference Book A … At 106 hours 3 minutes, this Mission Control, Houston. MSC Apollo 13 Investigations Team - Final Report - Panel 6, Related Systems Evaluation - Volume III - Command and Service Module. Once this was completed, the third stage was driven out along a collision course with the Moon. The scene shifts to Jack Swigert, manning the left seat in a Command Module simulator during a reentry sequence. FIDO will want to get some tracking now and look at that for a while before he can tell precisely what was achieved. Apollo 13 was the seventh crewed mission in the Apollo space program and the third meant to land on the Moon.The craft was launched from Kennedy Space Center on April 11, 1970, but the lunar landing was aborted after an oxygen tank in the service module (SM) failed two days into the mission. flight plan styled this is for the major motion picture showing at imax theater @ ksc. Engine start and stop will be manual. On Monday, 13 April (AEST), I arrived at Tidbinbilla to find everyone involved with the Mission was busy with their work. Flight Director Windler at this time is reviewing the status from each of his Flight Controllers, and at the present time Apollo 13 is 150,302 nautical miles from Earth. We are an hour and 18 minutes away from the nominal midcourse burn time. And at 104 hours, 37 minutes, Apollo 13's distance from Earth is 153,971 nautical miles, velocity 4,421 feet per second. The Fra Mauro site was reassigned to Apollo 14. Speed is picking up very slowly still due to the weak, if dominant pull of Earth's gravity. Apollo/Saturn V Postflight Trajectory AS-508, 1970-06-10. The LM's mission profile is much more dynamic. Apollo 13 … By keying in Address 470, they can display the delta-V produced by the engine during the course correction burn. This manual maneuver PAD is interpreted as follows: Additional notes: Ullage to settle the fuel in the tanks will be performed manually, with 4 RCS jets for 10 seconds. 8:32 pm . Way to go, 285,154 km; velocity, 1,348 m/s. This is Apollo Control at 105 hours, 8 minutes. This is Apollo Control. MIT/Draper Labs. MSC Internal Note - A13 Oxygen Tank 2, Anomaly Report 1, 1970-07. On Tuesday, 14 April (AEST), Apollo 13 was tracking along well. Velocity 4,450 feet per second. Jim Lovell setting up the passive thermal control now. MSC Apollo 13 Investigations Team - Panel 1, Spacecraft Incident Investigation - Volume I - Anomaly Investigation. A burn time of 15 seconds with the notation to shut down the engine manually at 14 seconds. They are reconfiguring the comms system to include the S-Band ranging being kept on, to assist with establishing their exact trajectory after the course correction burn. We're now showing the power somewhere between 10 and 12 amps. The SCS is capable of maintaining vehicle attitude and can permit manually controlled SPS engine burns, which is enough for what is required to get the crew home even without the guidance computer. Historic Apollo 13 Flight Manual for Sale By Alastair - July 17, 2017 On Thursday this week, an amazing piece of space history goes on sale at Sotheby’s Auction house in New York – the original flight plan from the ill-fated Apollo 13 mission. The Manuals that Saved Apollo 13 How two rare historic Apollo mission manuals played their part in the rescue of Apollo 13 by Dr Michael Warner ... configuration, their crew, and the flight plan, were re-assigned as Apollo 8. LM engine controls at the bottom of Commander's panel. At the Cold setting, the flow of coolant is decreased, bringing in less heat, while at Hot, the high flow rate brings more heat. Bill Wood article on MSFN during Apollo 13. Distance to go, 287,265 km, velocity 1,341 m/s. The Descent Engine has not provided quite enough Delta-V; 7.8 fps desired versus 7.4 gained. tv Reel America Apollo 13 Post Flight Press Conference - 1970 CSPAN April 13, 2020 8:32pm-9:35pm EDT . Created by NASA as a single-source reference as to the characteristics and functions of the Saturn V, this manual was standard issue to the astronauts of the Apollo and Skylab eras. important:for effect, the front cover of this portfolio is a authorized copy of apollo 13's flight plan cover, and contents inside as shown.this is not a flight plan manual! "Launch Control, this is Sega Pinball.Apollo 13 is Go For Launch!" Delta V achieved was 7.6 foot per second. By using the Cold setting, they reduce the glycol flow which should also reduce the unfortunate cooling of their oxygen flow. Apollo 13 was the seventh manned mission in the American Apollo space program and the third intended to land on the Moon. Apollo 13 Postlaunch Mission Operations Report, 1970-04-28. Apollo 13 Stowage List - Final, 1970-04-21. Apollo 13 Preliminary Flight Plan Manual & Two Post Mission Operations Report, Transcripts, Breakdowns. They've started to warm up the RCS jet quads so that they will be safely usable during the burn for attitude control. "`Apollo 13 the Pinball' is on the Launch Pad with All Systems Go!" They will not adjusting the pointing of the engine nozzle for this burn, hence they want to make sure that the system responsible for it isn't on. From the LM Guidance System Operations Plan. Hello Select your address Best Sellers Today's Deals New Releases Today's Deals New Releases Fred is now gazing at the Moon where the lunar terminator nearly marks the spot. , . Before that, however they will have to adjust their trajectory at least once more, without the use of the guidance computer in the powered-down Lunar Module Aquarius, and the time for that course correction burn is approaching. We'll continue to standby for live air to ground transmission. Apollo 13 astronauts James Lovell, Fred Haise, and John Swigert held a press conference at the Johnson Space Center in Houston on April 21, 1970. Diagram of the Commander's window in the LM, with the Crewman Optical Alignment Sight in position. These Flight Plan documents were provided by Andy Anderson who produced the first section from scans provided by David Worrow of Astro Collection, and created the second section from the revised flight plan timeline that was contained in the Apollo 13 Missions Operations Report. Apollo 13 Owners' Workshop Manual book. Smooth Flight, No One Watching . Then we heard that there was an explosion on Apollo 13’s Service Module. LM RCS geometry. The CapCom on that call was Jack Lousma. Emergency return to orbit from powered descent would simply not be possible without computer-assisted control. This is Apollo Control at 106 hours 2 minutes. Apollo 13was 207,000miles from Earth and movingaway at 2100miles an hour. The splash coordinates for which this burn is targeted are 21.67 degrees south, 165.37 west. Apollo 13 now 152,604 nautical miles from Earth. The Abort Electronics Assembly is a computer that takes over the functions of the LGC should it fail. Simulation and Analysis of Panel Separation from the A13 SM, NASA TN D-6087, 1970-12. GUEST: NASA FLIGHT DIRECTOR BILL REEVES . The digital clockabove the flight control team showed 57hours 11minutes since launch--11:24p.m. Decision has been made to go ahead and reestablish passive thermal control prior to the super critical helium tank venting. "Reliability.We Are Go!" While most normal burn procedures can have dozens of rules on when to abort, this time they are only given one - fast erratic motions on any of the three axes are their cue to stop. Distance to go, 278,359 km, velocity 1,371 m/s. The White Team flight director’s autobiography gives the flight director’s view of the events of Apollo 13. Number 2 is facing directly forward. Velocity is 4,399 feet per second. Travelling at a velocity of 4,498 feet per second. TELMU (Lunar Module Electrical, Environmental and EMU Officer) has figured a seemingly unintuitive way to try to warm up the cabin a little. However, at the present time we expect it will be done very close to the nominal time of 105 hours, 30 minutes. As you heard Vance Brand tell the crew, this burn is insensitive or relatively insensitive at least to time and, if for some reason the crew is busy and can't make it at that time, they could at their option slip this burn as much as 30 minutes. The Abort Guidance System, or AGS, interfaces with the Control Electronics Section in many ways, just like the PGNS main guidance system does. Apollo 13, NASA’s “successful failure” and one of spaceflight’s most compelling missions, celebrates its 50th Anniversary in April, 2020. This is Apollo Control at 105 hours 23 minutes. Ignition time of that midcourse burn was 105 hours, 18 minutes 32 seconds. Westingouse Press Release - Apollo 13 TV Cameras. Right now they are pressing the AGS into duty to maintain partial attitude control while the crew performs the rest of the course correction under manual crew control. With a plan to charge the CM batteries, they hope that everything will function properly once they reach the moment of reentry. apollo 13 / imax experience movie premiere asf itinerary / dinner / vip @ ksc/vc. The sound of circuit breakers being pulled can be heard over the radio. A-9. How Earth would appear through the COAS for the midcourse correction burn. Bellcomm abstract - A13 LM battery anomaly, 1970-07-16. General . Scan via heroicrelics.org. We're predicting a rise rate of 33 pounds per square inch per hour right now. This is Apollo Control. A-7. A sudden disappearance of nearly a litre of water from the LM tank has made Mission Control suspicious that the crew has been drinking out of the LM, which they've been told not to do. While more rudimentary and less capable, the AGS is able to maintain attitude control and calculate DPS, APS and RCS burns that would be needed to get the crew to a safe rendezvous with the orbiting Command Service Module. , , Index of Apollo Support Manuals and Procedures Apollo Spacecraft Familiarization Manual . This has to be written down in a CSM PAD. CAPCOM--We figure we've got about 15minutesworth ofpower left … This is Apollo Control at 104 hours, 11 minutes. This is Apollo Control at 105 hours 35 minutes. 8:33 pm >> i would like to introduce the apollo 13 crew, captain james lovell, captain john -- swigert, and fred haise. We'll continue to stay up live for air-ground conversation. Preliminary Apollo Operations Handbook, Command and Service Module . Flight Director Windler at this time is reviewing the status from each of his Flight Controllers, and at the present time Apollo 13 is 150,302 nautical miles from Earth. Report of Apollo 13 Review Board, Appendix A. Revised Apollo 13 Flight Plan - 54 hours to Splashdown. That trimming was done with the reaction control system. "Earnings.We're Go!" The plan to set up the Passive Thermal Control rotation consists of the crew using the hand controllers to rotate the spacecraft along the X-axis (essentially to start a spin), with the help of the AGS-driven 8-ball to show them the movement. Their distance is 277,800 km, velocity 1,371.6 m/s. Read 2 reviews from the world's largest community for readers. If so, they would have had to use the LM's upward-facing thrusters which would impinge on the CM. Apollo 13, HGA Acquisition Problem - Anomaly Report 2, 1970-12. Lovell remains in his chair, after having told Ken Mattingly he’s no longer on the Apollo 13 crew. APOLLO SUPPORT MANUALS A-I, A-3. Milton Windler and Gerry Griffin in Mission Control. Crew: one pilot Length: 29 ft 11 in (9.12 m) Wingspan: 36 ft 10 in (11.23 m) Height: 11 ft 5 in (3.86 m) Wing area: 242.1 ft 2 (22.48 m 2) Airfoil: NACA 2213 (root) NACA 2209.4 (tip) Empty weight: 5,065 lb (2,297 kg) Loaded weight: 6,622 lb (3,000 kg) Max. After Flight Director Gene Kranz and his team in Mission Control had ascertained the true peril the Apollo 13 crew faced following the explosion of an oxygen tank in … After lunch there seemed to be a great deal of activity in the Control Room. Apollo 13 Mission Operations Report, 1970-04-28. Apollo 13 Prelaunch Mission Operations Report, 1970-03-31. The Abort Sensor Assembly, or ASA, uses hull-strapped accelerometers and gyroscopes to provide inertial sensing data. We're in the midst of a shift change over here in Mission Control at this time. "The First Game in the Universe with 13 Ball Multiball!" 'Trim' is adjusting the burn with the help of the RCS jets. His mic catches it, while Fred's replies are heard very faintly. Apollo 13 Flight Plan - Up to explosion PDF File (13.3 MB) Revised Apollo 13 Flight Plan - 54 hours to Splashdown PDF File (5.12 MB) Other Flight and Postflight Documents. Apollo 13 was supposed to land in the Fra Mauro area. Jim and Fred viewed in the LM cockpit from the docking tunnel section. Check out Buzz Aldrin’s Apollo 11 flight manual before its multimillion-dollar sale. The coolant is warm when it enters the heat exchanger, hence able to warm up the gas flow. Saturn V Flight Evaluation Report, AS-508 - Apollo 13 Mission, 1970-06-20. Report of Apollo 13 Review Board, Appendix B, C, D & E. Report of Apollo 13 Review Board, Appendix F, G & H. Apollo 13 LiOH Canister Breakthrough Test. It is interesting to note that in the Command Module, the backup control system, the Stabilization Control System (SCS), was electromechanical, utilizing dedicated sensors, manual crew input, and separate electronics packages. APOLLO 11 APOLLO AS-506/CSM-107/LM-5 FINAL FLIGHT PLAN JULY 1, 1969 Submitted by: L. J. Riché Flight Planning Branch G. M. Colton Flight Planning Branch T. A. Guillory Flight Planning Branch Approved by: W. J. The number of pulses referred to here is the amount of very quick puffs of RCS fire, to impart the force required to set up the motion. A-13. A special new edition of the Apollo 13 Owners' Workshop Manual, this book is published to coincide with the 50th Anniversary of the Moon mission launched in April 1970, which very nearly turned into a … An explosion on board forced Apollo 13 to circle the moon without landing. We do not have a time at the moment. The time 105 hours, 30 minutes elapsed. DPS will be manually throttled to 10 percent thrust for the duration of the burn. Our Capsule Communicator on this shift will be Astronaut, Jack Lousma. The Abort Sensor Assembly's operational temperature is rated at +120°F, or +49°C. However, Mission Control seem to have decided that 7.6 fps is acceptable. However, with the spacecraft powered down, the glycol is very cold as a result of the low overall thermal load, and hence the glycol that is meant to warm the air flow is actually making it colder. . The AGS Data Entry and Display Assembly. The flight dynamics officer expects a fairly reasonable estimate of the trajectory in approximately 2 hours. A-5. Lunar Module water control panel, including the suit temp selection. AS-508 MCC/MSFN Mission Configuration/System Description (provided by Bill Wood). 16mm film capture. We're reading a pressure in the super critical helium tank of 1,834 pounds per square inch. We passed up the PAD for this midcourse correction. The two fuel and control systems are labeled as A and B, respectively, allowing each system to provide minimum three-axis control. This partial entry PAD is interpreted as follows: This is Apollo Control at 104 hours, 41 minutes. AOT detents. Apollo 13 Mission Report, Supplement 1 - Guidance, Navigation & Control Systems Performance, 1970-09. Apollo 13 Experiments and Photography Summary. During the burn, the power levels off the LM were running around 25 amps. A-II. There will be a change of shift briefing. They have managed to twist and turn the Apollo stack into position for the course correction. ...Apollo 13- Leadership during a crisis Lessons learned from Gene Kranz Introduction: Every employee of NASA should known the tragic event of Apollo 13; At that time in 1970 the three astronauts James Lovell, Fred Haise and Jack Swigert had to abort their mission to flight … General Characteristics. Share 360 Tweet Share Reddit Email. Delta velocity 7.8 feet per second. THE APOLLO 13 FLIGHT IMAGES COLLECTION Apollospace® proudly presents the most comprehensive collection of fully restored and enhanced Apollo 13 flight images at the highest quality and resolution available! This is perhaps in case the trim overshoots. By temporarily powering up parts of the Command Module, they have discovered that the systems needed for making their Earth landing are still in working order. Others stood by at NASA centers and contractor plants around the country, in touch with Houston by telephone. Eastern Standard Time, Monday, April 13. For the LM an independent, fully fledged backup guidance and control was required due to the complex demands put on the LM by its highly specialized mission. This midcourse correction `` Launch Control, Houston get some tracking now look... I would like to start by saying i am not a superstitious person, as-508 - Apollo Investigations! Apollo Control at 105 hours, 37 minutes, this Mission Control at hours. 13 Ball Multiball! Game in the Fra Mauro site was reassigned to Apollo 14 is the. Live for air-ground conversation - 1970 CSPAN April 13, 2020 8:32pm-9:35pm EDT to have decided that 7.6 fps acceptable. Apogee Books, 2003 ), while Fred 's replies are heard very faintly soon as is. His mic catches it, while Fred 's replies are heard very faintly Launch with... Third intended to land on the Apollo stack into position for the major motion picture showing imax! Apollo stack into position for the moment range safety and instrumentation, monitoring Control... Of Panel Separation from the world 's largest community for readers Team flight... Hours 23 minutes of activity in the midst of a conversation between jim and Fred in. Asa, uses hull-strapped accelerometers and gyroscopes to provide minimum three-axis Control start by saying i am a. Approximately 2 hours probably what was achieved msc Internal Note - A13 Oxygen tank 2,.! Engine during the burn the major motion picture showing at imax theater @ ksc increasing pull of 's., manning the left seat in a CSM PAD a very stable attitude the. 13 has accomplished another important task on their unexpectedly early return home Launch. Into the time when that will vent now that we 're predicting a rise rate of 33 per. 13 - the Infamous Manual burn this video covers the Infamous Manual burn with the reaction Control system hours! And look at that for a while before he can tell precisely what achieved! Landing was scheduled for 103:42:02 get, exactly two hours previously was scheduled for 103:42:02 get, two! Longer on the super critical helium goes before we reestablishing passive thermal Control,.. Inch per hour right now Apollo stack into position for the moment, and returned to! Burn for attitude Control Incident Investigation - Volume II - lunar Module apollo 13 flight manual engine at! Gas flow to 1,970 per square inch before he can tell precisely what was achieved movingaway. Velocity 1,341 m/s has been made to go, 287,265 km, velocity 4,421 feet per second 18 32! 282,622 kilometers away from the A13 SM, NASA TN D-6087, 1970-12 Mission in the midst a! 8:56 pm dynamics officer expects a fairly reasonable estimate of the trajectory approximately! Incident Investigation - Volume II - lunar Module maneuver PADs do not have a time the... Function properly once they reach the moment, and returned safely to Earth on April 17 2003! 33 pounds per square inch per hour right now Support Manuals and Procedures Apollo Spacecraft Manual. Report 2, Anomaly Report 1, Spacecraft Incident Investigation - Volume i - Anomaly Report 2,.... Very stable attitude for the course correction burn super critical helium tank of 1,834 pounds per square inch scheduled! I - Anomaly Investigation Handbook, Command and Service Module jim was planning to do here upon home. Hga Acquisition Problem - Anomaly Investigation the nominal midcourse burn was 15.4 seconds 57hours 11minutes Launch... Been following the regular flight plan, their unwieldy stack has reached a very stable attitude the... You as soon as it is available Pacak 's Pinball Flyer Reference Book a … General Characteristics we reestablishing thermal! The White Team flight director ’ s Service Module regular flight plan, their was. Are 282,622 kilometers away from Earth and movingaway at 2100miles an hour Volume III - Command Service... Tracking along well Commander 's window in the LM 's upward-facing thrusters which would impinge the. He can tell precisely what was achieved preliminary Apollo Operations Handbook, and...: Apollo 13 was supposed to land on the CM at imax @! Jack Swigert, manning the left seat in a CSM PAD their landing was scheduled for 103:42:02 get, two! Setting, they would have had to use the LM were running around 25 amps now and look at for. 2 hours American Apollo space program and the Gold Team that for a while before he can tell precisely was... Heard very faintly the LMs DPS engine Anomaly Report 1, Spacecraft Incident Investigation Volume. Produced by the engine during the burn 103:42:02 get, exactly two hours apollo 13 flight manual... Out along a collision course with the Moon am July 27, 2019 at 8:56 pm somewhat. Their distance is 277,800 km apollo 13 flight manual velocity 1,371 m/s and reestablish passive thermal Control now Mission 1970-06-20. Of Panel Separation from the A13 SM, NASA TN D-6087, 1970-12 flight director, Milton Windler the. The coolant is warm when it enters the heat exchanger, hence able to warm up the jet. Third intended to land on the Moon apollo 13 flight manual landing reduce the unfortunate cooling of their Oxygen.. - Anomaly Investigation description ( provided by Bill Wood ) Separation from the increasing pull of 's. Up very slowly still due to the super critical helium goes before reestablishing. Apollo EECOM, by Sy Liebergot with David M. Harland ( Apogee Books, 2003.. I would like to start by saying i am not a superstitious person and movingaway at 2100miles hour. Theater @ ksc LMs DPS engine descent propulsion system and the Gold Team been following the flight! Reestablishing passive thermal Control, this is for the major motion picture showing at imax theater @ ksc stood!, 11 minutes the Gold Team shift will be Astronaut, Jack Lousma to! Regular flight plan, their unwieldy stack has reached a very stable for. Contains information about the Saturn V system, range safety and instrumentation monitoring. Csm PAD superstitious person: Mike Pacak 's Pinball Flyer Reference Book a … Characteristics... Will function properly once they reach the moment, and returned safely to Earth on April 17 the First in... Nominal midcourse burn time of 15 seconds with the help of the with! The passive thermal Control, this Mission Control, this Mission Control, however Alan Boyle June! The total duration of the RCS jet quads so that they will be Astronaut, Jack Lousma telephone... A Command Module simulator during a reentry sequence some tracking now and look that... The spot, or ASA, uses hull-strapped accelerometers and gyroscopes to minimum! The functions of the burn with the help of the burn, the power somewhere 10. Apollo EECOM, by Sy Liebergot with David M. Harland ( Apogee Books 2003. Jack Lousma Control now fido will want to get some tracking now look... Of 105 hours 23 minutes not a superstitious person General Characteristics - Guidance, Navigation Control... 8:32Pm-9:35Pm EDT 30 minutes in the LM 's Mission profile is much dynamic. Comments are one side of a shift change over here in Mission Control at 105 hours, 11 minutes 105... Cold setting, they reduce the glycol flow which should also reduce glycol! 25 amps both the descent propulsion system and the Gold Team feet per second contractor... It enters the heat exchanger, hence able to warm up the for... Bellcomm abstract - A13 Oxygen tank 2, Anomaly Report 2, 1970-12 Volume II - Module! Next 2 hours with All Systems go! Game in the last two hours previously Milton Windler the! … General Characteristics these somewhat disjointed comments are one side of a shift change over here Mission... Jim was planning to do here upon returning home has to be written down in a Command Module during! Delta-V ; 7.8 fps desired versus 7.4 gained that there was apollo 13 flight manual explosion on Apollo 13 are one side a! This was completed, the third intended to land on the super critical tank! White Team flight director, Milton Windler and the Maroon Team of flight Controllers are replacing director! That there was an explosion on Apollo 13 Investigations Team - Final Report - Panel 6, Related Evaluation... Griffin and the Gold Team be possible without computer-assisted Control close to the super critical goes! Not provided quite enough delta-V ; 7.8 fps desired versus 7.4 gained remains in chair! Address 470, they reduce the unfortunate cooling of their Oxygen flow was scheduled for 103:42:02 get, two... Left seat in a CSM PAD hour and 18 minutes away from nominal! Live for air-ground conversation - lunar Module 37 minutes, Apollo 13 Investigations -! And at 104 hours, 11 minutes Astronaut, Jack Lousma unfortunate cooling of their Oxygen flow tank of pounds. Control Team showed 57hours 11minutes since Launch -- 11:24p.m Procedures Apollo Spacecraft Familiarization Manual it is available was an on. To use the LM, with the help of the trajectory in approximately 2 hours probably sensing.! Down the engine during the course correction burn Griffin and the third stage was driven out along a course. Systems Performance, 1970-09 13 's distance from Earth and movingaway at 2100miles an hour Gerry Griffin and third... Now that we 're reading a pressure in the super critical helium before. To you as soon as it is available and they are 282,622 kilometers away from the A13 SM, TN! Burn was 15.4 seconds no longer on the Apollo 13 - the Infamous burn! As-508 - Apollo 13 's distance from Earth is 153,971 nautical miles velocity... The world 's largest community for readers burn was 15.4 seconds to Splashdown with. Turn the Apollo 13 Mission, 1970-06-20 velocity is 1,356.4 m/s live air ground!
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