“But if you turned off the byplay between Mission Control and the Sea of Tranquility, with its deliberately mundane and routine chatter, and stared into that black-and-white television monitor, you could glimpse that we humans had entered the realm of myth and legend.”
Part II: The Gift of Apollo
Chapter 6: We are the First, We won’t be the Last.
“I’m coming back in… and it’s the saddest moment of my life.”
- Ed White, Gemini IV EVA.
(Debby Reynolds, Belly up to the bar, boys)
Apollo faced major hurdles and redesigns following the December 12th accident. Easily the most time consuming change was the reversion back to North American’s original mixed gas atmosphere. This switch made a rapid and spontaneous fire like that of Gemini 6a a near impossibility. Additionally, further fire prevention was taken by replacing nearly all flammable materials within the spacecraft with fire-retardant alternatives.
Ultimately these changes affecting the CSM, LM and EVA Suits would be severe; However their benefit would far outweigh any delays to the Apollo program, as engineers at NASA could proceed knowing this was the safest version of a very dangerous endeavor. Landing men on the lunar surface and returning them safely to the Earth was to be mankind's greatest engineering challenge to date, and this was partially helped by Apollo’s unique flight scheme.
When Project Apollo was originally pitched in 1961, contractors and mission planners had expected to use a mission mode called direct descent. This mode would merge the lunar lander and reentry vehicle into a singular behemoth of a spacecraft, allowing the mission to circumvent pesky rendezvous’ and dockings. This was the mode of choice when North American was chosen in November of that year to proceed with construction of the Apollo spacecraft.
However the Gemini Program had gotten these once complex maneuvers down to an exact science; and even by 1962 (notably many years prior to the first Gemini mission) NASA management was beginning to come around to Grumman’s mission mode of choice: Lunar Orbit Rendezvous (LOR). This mission mode would allow the entire spacecraft to ascend from the Earth to the Moon atop a single Saturn V rocket, and would counterintuitively simplify the mission. This, however, caused an issue with North American’s in-development Apollo spacecraft: it would have to dock.
(Apollo Direct Descent Concept, North American, 9-12-61)
Before NASA committed to LOR in July of ‘62, the Apollo Spacecraft wouldn’t have docking capabilities. This meant the capsule would have to see major redesigns to the nose area, allowing crew to egress through a pressurized docking tunnel to the now-dedicated lunar vehicle. This led the Apollo designers to favor a two step approach, where they would first develop the capsule and service module, then the docking mechanism and tunnel. This led to two distinct versions of the Apollo CSM, Block I and Block II. Following the December 12th incident, both capsules would yet again see major redesigns and be dubbed Block IIA and Block III respectively.
Block IIA would carry no docking mechanism or pressurized tunnel, and would instead fly with a simplified nose-cone shell, protecting its parachutes during ascent and reentry. This simplified spacecraft would fly four times on Apollo’s 1-4 with all further missions switching to the docking capable Block III. This would ultimately allow NASA to test out the Apollo spacecraft in Earth orbit multiple times before pursuing a lunar landing, while not interfering with their already crammed schedule. Apollo 1, the first crewed mission of the program, was scheduled to lift off in September of ‘67.
Apollo 3 would beat them to the launchpads however, lifting off on August 14th, 1967. This mission reveals a unique quirk of NASA’s naming schemes that carried over from the Gemini Program; Missions were to be numbered in the order in which they were scheduled, not the order in which they flew. As such, Apollo 3 was to be the first all-up test of the Saturn V launcher.
AS-501 lit her engines with a roaring thunder, louder than any of humanity's machines to date, excluding the atomic bomb. The gargantuan rocket rose into the air atop a pillar of soot, as the engines glowed with the light of the sun. Engineers and onlookers alike cheered as the rocket's engines crackled and roared, and Mission Control declared over the loudspeaker: Apollo 3 has cleared the Tower!
Apollo 3 accelerated as it traveled further into the sky, rapidly approaching Max-Q, the point of maximum aerodynamic pressure on the vehicle. As it was crossing Max-Q, the oscillations began; The vehicle had entered a self-perpetuating cycle of acceleration changes the the engineers had coined Pogo-Oscillations. These oscillations would go largely unnoticed until a minute or so after staging occurred. The S-IC flamed out as the S-II’s interstage motors fired, sending the second and third stages further up and away from the giant first stage.
Mark seven minutes… forty four seconds and we are receiving data showing the premature shutdown of two of the second stage engines.
Despite this failure, the Launch Vehicle Digital Computer (LVDC) adjusted course and began a steeper trajectory. The S-II burned longer and further downrange than anticipated, leaving more work to be done by the rocket’s third stage to reach orbit.
We have shut down of the 3 J-2’s and we are expecting staging shortly.
The S-IVB roared to life, seemingly unscathed by the cascading series of failures below it, the final J-2 engine slowly spooling up to its full, rated thrust. The stage performed nominally as it performed its short burn, ultimately placing Apollo 3 into a stable, albeit more elliptical than desired, orbit.
Apollo 3 completed 3 orbits before successfully deorbiting, reentering and splashing down in the Pacific. This mission would prove the Apollo spacecraft safe for manned flight, while also proving NASA still had some problems to solve with the Saturn V. This was, while not ideal, a good outcome for NASA. Schedules would not need to be changed, and a second unmanned test of the Saturn V, Apollo 5, was scheduled for Q1 1968.
For the time being, Mission Control had more pressing matters. AS-204, Apollo 1, was to be the first manned mission of the Apollo Spacecraft. Her crew consisted of 3 of NASA’s best and brightest. Command Pilot Gus Grissom had been one of the first Americans to fly into space, as well as the first to command the Gemini Spacecraft on Gemini 3. Senior Pilot Ed White was the first American to walk in space on his first mission, Gemini 4. Lastly the mission carried one rookie astronaut, Roger Chaffee. Despite his rookie status, he had been at the consoles of mission control numerous times, and had proved himself more than capable in the simulators.
(Chaffee at the consoles of Gemini 3)
Gus Grissom, the most experienced of the three, was also seen as something of a troublemaker at NASA. He named his Gemini capsule Molly Brown after
The Unsinkable Molly Brown in hopes to avoid his capsule sinking as it had on
Liberty Bell 7. While comedic, this did not go over well with NASA personnel, who swiftly banned the practice of naming spacecraft.
This ban, however, would not last forever. Apollo 1’s crew pled to name their capsule Phoenix, in honor of, as Ed White put it Apollo’s rise from Gemini’s Tragic ash. This idea was rather well received by mission control and NASA personnel alike, and in May of that year, NASA’s Associate Administrator James Webb approved the name, on one condition. Future capsule names were to be safe for broadcast, and they couldn’t paint the administration or their goals in a bad light. And with this, CSM-101 dawned the name Phoenix, and was awaiting her final preflight check: the plugs out test.
It was warm and humid as the astronauts arrived at the Cape. The warm pre-sunrise glow dimly illuminated the Floridian coast, as the three walked to the suit-up room. The crew donned their A1C suits with help from support teams, and prepared themselves for the challenging simulation ahead.
(Chaffee seen here wearing the A1C Pressure Suit)
The A1C took the majority of its design from the Gemini-Era G4C suit. As such, it was far simpler than the later suits destined to walk on the lunar surface; However it was the right fit for the mission. The A1C offered the life support and reliability necessary to perform a LEO flight, and even an EVA if the mission required it.
The astronauts exited the crew quarters and began the walk to NASA’s newly purchased, and extensively modified Clark-Cortez motorhome called the Astronaut Transfer Van, or AstroVan for short. The three astronauts disembarked the van at the launch pad, wiping the fog from their visors and staring up at their Saturn IB in awe.
Grissom: She’s a hell of a beauty, isn’t she?
White: Sure is…
Chaffee: This is really somethin’ else.
The astronauts boarded the elevator up to their vehicle, and entered the white room. Today’s schedule was to be the most complex in the three astronauts’ careers. It would put them through the paces of flying the most complex manned spacecraft ever built, and prove their aptitude thorough enough to fly. The three men boarded Phoenix, helped by a swarm of launch personnel. Once the astronauts were seated, and final checks were performed, the hatch was sealed, and the clock started. Their extensively redesigned Block-IIA spacecraft had been proven for flight months prior. Now it was her crew’s turn.
Nearly as soon as the test began, so did Mission Control’s difficulties. Shortly after disconnecting the capsule, Capcom found it nearly impossible to hear her crew. Following multiple blackouts in communications, and an almost complete breakdown of the test schedule, both the astronauts and mission control were fed up.
Grissom: How are we gonna get to the Moon if we can’t talk between three buildings?
White: They can’t hear a thing you’re saying.
Grissom: Jesus Christ…
…
Capcom: Come again Gus?
Grissom: I said how the hell are we planning on landing on the moon if we can’t talk between two or three buildings?!
Chaffee: Here we go…
Grissom: I mean seriously, you need to get your shit together so we can get this show on the road, Houston.
And get their shit together they did. Shortly after Gus made his remark, in a fit of frustration, Gene Kranz called off the test. The spacecraft was to be rolled back to the Operations and Checkout Building that evening and wasn’t to leave until
this little comms issue of theirs was fixed.
It took a few days, but after hours of digging around under the seats of Pheonix, a bundle of frayed wires was found under Gus’s seat; This ultimately was found to be preventing the spacecraft’s antennas from broadcasting at full strength. After some minor checkouts, the Apollo capsule was readied for testing once more. She was scheduled to be rolled out the following morning, the 16th of August, 1967.
(Phoenix being mated to the Spacecraft Adapter)
Capcom: Good Morning Phoenix, how do you read?
Grissom: Loud and clear Capcom!
Mission control ran the crew through their paces, simulating all manner of failures in their spacecraft leading up to launch; However the crew kept her steady. They did exactly what they needed to to maintain the flight schedule and correct the flight computer’s errors. The three astronauts had performed perfectly, and proven their proficiency with the Apollo. Phoenix and her crew were ready for Apollo’s maiden voyage.
Public Affairs Officer: This is Apollo Saturn launch Control at T minus 22 minutes and counting. T minus 22. We are standing by for the next major milestone before flight as the Commander of the Apollo 1 spacecraft, Virgil Grissom, will go through a series of test firings of the spacecraft's Reaction Control Systems. These are the engines located in clusters of four circling the spacecraft’s Service Module; Each engine is capable of outputting some 100-pounds of force (~445N) to allow the spacecraft to rotate about its axi in orbit.
Public Affairs Officer: This is Apollo Saturn launch Control at T minus 17 minutes and counting. T minus 17. All signs show we are go for launch at this time. The weather here on the floridian coast is a balmy 81 degrees, with beautiful blue skies. Winds are trending towards favorable, sitting at about 10 miles per hour to the East. We appear to be go for launch!
Grissom: Sheesh, glad we have air conditioning in this thing…
Chaffee: You bet.
Public Affairs Officer: This is Apollo Saturn launch Control. We're at 8 minutes… 45 seconds and counting as Spacecraft Test Conductor Skip Chauvin is going through a final status check with the spacecraft team here at the KSC. Teams are monitoring the performance of the Saturn IB, and all pressures seem to be nominal, we are go for launch as we are closing in on 8 minutes to liftoff, T minus 8 minutes and counting. This is Launch Control.
Public Affairs Officer: This is Apollo Saturn launch Control at T minus… 3 minutes and counting, we are continuing the countdown. The three astronauts have just completed the final checks of their guidance and navigation systems.
White: Okay Capcom, I can confirm we are running program 2, I repeat running P-02, Verb 75.
Capcom: Copy that, Ed. Good to hear, y’all holding up okay?
Grissom: No complaints here houston!
Phoenix’s Computers were now running internal guidance, and all was set for the launch of Apollo 1. The spacecraft sat in the low hanging floridian sun, seemingly glowing with all the ingenuity of mankind up to that point. Her crew wasn’t going to the moon, not even close. But they understood that with this small step, they’d be placing humanity one giant leap closer to that daring goal.
Public Affairs Officer: This is Apollo Saturn launch Control coming up on T minus One minute and counting; Mark. T minus sixty seconds. Atmosphere is internal and guidance is internal. All reports are coming in good as we approach T minus 50 seconds. Coming up on the forty second mark; Mark. T minus forty and counting.
Public Affairs Officer: Forty, all reports coming out of the blockhouse appear good as we converge on the T minus- Mark; T minus thirty seconds to liftoff of Apollo 1. The Saturn IB launch vehicle weighing in in excess of 1.3 million pounds is now ready as we close in on the ten second mark.
Capcom: Standby for the 10-second count.
Grissom: Roger-
Capcom and Public Affairs Officer: T minus 10… 9… 8… 7… 6… 5… 4…
Capcom: We have Ignition! 2… 1…
Public Affairs Officer: Liftoff! Liftoff of Phoenix towards the Heavens!
White: Yahooo!
Chaffee: Alright!
Grissom: Liftoff Houston- Clock’s runnin’
AS-504 lit her 8 H-1 engines as the Florida coast received their wakeup call. It was showtime. The rocket rose up off the pad as onlookers screamed out in cheers and awe. Phoenix was on her way, and by extension, so was the Apollo Program.
Grissom: Alright Capcom, we got a roll program!
Public Affairs Officer: 12 seconds after liftoff and we have report of a roll program!
Capcom: Roger roll, Phoenix.
The rocket rolled, slowly but surely, lining up the rocket to her 32 degree inclination before beginning the pitch program. The S-IB was performing flawlessly, as it had for the previous flights.
Grissom: Okay Houston, Pitch is looking good on our end
Capcom: Roger Pitch, Gus.
Public Affairs Officer: As we approach 1 minute into the flight, we are getting reports back from the crew that the roll program has suspended, and the computer is back in mode 1. This indicates that in the case of an abort, an extra pitch motor on the launch escape tower would fire to help the crew clear the fireball and splashdown off the coast.
Public Affairs Officer: We are coming up on 2 minutes; Mark, 2 minutes. Status checks show the crew is go for S-IVB staging.
Capcom: Go for Staging, Phoenix.
White: Roger that, go for staging.
Grissom: Inboard cutoff, smoothing out a bit. Okay we have outboard engine cutoff.
Capcom: Roger that Gus, proceed with staging.
The S-IVB separated gracefully from the stage below it as the three ullage rockets fired. Fractions of a second after this event, the propellant settled in the aft of the tanks, and their J-2
roared to life
Grissom: Let’s see what this baby can do! We got good light on that J-2 Houston!
Capcom: Glad to hear Gus, Expect to see tower sep here in about T minus 20.
Public Affairs Officer: We’re here at T-plus two minutes… thirty seconds and the crew has lit their second stage engine, expect to see that launch tower on top of the capsule shoot off shortly.
Chaffee: Okay Flight, that tower really shot off. [Unintelligible] Miles and miles!
Capcom: Glad to hear it’d save your skins if we needed it. You’re go for mode 2 Phoenix.
Grissom: Roger, mode 2.
Public Affairs Officer: We have clean tower separation here at T-plus 3 minutes, 5 seconds. Launch teams are reporting the S-IVB is performing nominally, and the flight computer has switched to a ‘Mode 2’ abort. This means the tower will no longer be needed, and the capsule would fire it’s RCS engines in the case of an abort.
Capcom: Okay 1, how do you read?
Grissom: We read you crystal clear flight.
Capcom: Okay we’re having some difficulties hearing y’all, try turning up the S-Band antennas.
White: Roger that, how’s this sound?
Capcom: A bit loud, but we’ll take it… I’ll go ahead and count you down at four… 3, 2, 1, Mark; All systems go at T-plus four, Phoenix.
Grissom: She’s a smooth ride Houston… Gimbal check looking good
Capcom: I’m sure Douglas’s glad to hear that, Gus; Roger good gimbal check.
Public Affairs Officer: We’re seeing slightly elevated heart rates sitting in excess of 100 beats per minute, this is to be expected and all physical parameters are within safe limits. The crews are experiencing 1G of acceleration at this point in flight, T-plus five Minutes.
The rocket was cruising brilliantly, and the three astronauts we’re having the ride of a lifetime, soaring up and beyond the sky at T+5 minutes into flight. G forces were relatively moderate all the way to orbit, at least by the crew’s standard. Both Grissom and White had seen G-Forces above 7 during the Gemini Titan II’s SECO, for the two experienced pilots this was nothing.
Chaffee: Bit of a bumpy ride flight-
Grissom: You ain’t seen nothing yet kid. We’re looking good for orbit at 9 flight.
Capcom: (laughing) Roger that Gus, prepare to switch to Mode IV in 35.
Grissom: Roger.
Capcom: Phoenix, your CMC and trajectory are go! Anticipate SECO here in 20.
Grissom: Roger… switching to mode 4
Grissom: Alright flight… we report SECO, zero-g and feeling great.
Capcom: Beautiful flight, Phoenix. Welcome to space.
Apollo 1 had reached orbit, clearing the first of many milestones for their mission. The 14 day mission was scheduled to put the spacecraft through her paces, ultimately displaying some of the scientific prowess of the program. However, days 1 and 2 of the mission were dedicated to the spacecraft itself; The crew would put the Command and Service Module (CSM) through its paces, as they had many times in the simulators leading up to flight.
White: Alright Gus, I’m gonna get these gimbals off
Grissom: Roger flight, we’re seeing Pitch 1 off, Yaw 1 off, Pitch 2 and Yaw 2 off as well. I repeat all 4 are off.
Capcom: Gotcha Gus, all 4 off. Beautiful.
White: Okay, DSKY is reading velocity at 25565; H-dot is minus four; and altitude is 122.3
Capcom: Roger that; Phoenix, your S-IVB has been safed.
The S-IVB began venting excess propellants, first hydrogen, then oxygen. By the end of the first orbit, the stage had vented almost all excess residuals, and the computer had been shut down. This left the booster safe for separation, and cleared the crew for at least 6 more orbits. The flight computer was reading their velocity at 25,565 feet per second [7,792 m/s] putting them just where they wanted to be.
White: okay flight, guidance is showing us at an apogee of 146, perigee of 135. (270x250km)
Capcom: Roger you loud and clear Ed; We copy your orbit, you guys are looking good down here.
Grissom: I got pretty good aim, don’t I?
Chaffee: -for an air force boy, yeah!
Grissom: Hey!
Grissom: Okay flight, how long until we can expect separation?
Capcom: Come again? We’re having a real rough time hearing ya down here Phoenix.
Apollo 1 was now drifting above the Atlantic, and despite some communications difficulties, was performing nominally. Mission control was trying everything they could to stabilize communications between them and Phoenix, and only by orbit 2 did they do so. Once comms were stable, the crew were go for separation, staging their spacecraft away from the now-safed S-IVB.
Capcom: Okay Phoenix, we got you good for staging.
Grissom: Roger that flight, we’re separating from the S-IVB now. Firing RCS and flipping around.
Chaffee: Isn’t she a beauty?
White: Sure is, no doubt about it.
Grissom: Okay flight, we’re sitting about 25 feet from the S-IVB, drifting away slowly.
Capcom: Glad to hear it, Phoenix
Apollo 1 went on to be yet another in a string of successes since the December 12th accident. The mission, clocking in just shy of 14 days, nearly doubled Gemini 7’s record of 8 days, a record set by NASA just two years prior. This mission showed that America was ready and eager to take on the challenge of going to the moon, while proving we had the tools to do so. Upon splashdown, after days of scientific research and humanities longest spaceflight to date, Gus Grissom put it best in a post flight interview:
Grissom: I mean that’s gotta be one of the greatest test-flights we could have asked for.
Apollo 2 (AS-205) lifted off a mere 48 days after Phoenix’s splashdown, proving that Apollo 1 wasn’t a one-off success. The mission largely repeated the 14 day success story of Phoenix before it, carrying new scientific instruments and collecting further data on the vehicle. The mission would provide training in the Apollo to a further three astronauts: Eliot See, Walter Cunningham, and Done Eisele.
Apollo 5(AS-502) would be the second mission of 1968, following Apollo 4’s LM testflight. The mission would see the Saturn V perform flawlessly after a number of minor modifications had been implemented to dampen the pogo-oscillations. It would be on this flight that NASA would test Saturn’s Trans Lunar Injection (TLI) capabilities for the first time.
Mission Control: Okay, we have burnout of the S-IVB, Apollo 5 is on her way to the moon!
The capsule would, as planned, simulate a critical emergency only 6 hours after TLI. This forced the CSM-201 to fire her main engine, performing a direct abort. This maneuver would provide a critical safety net, and be one of two methods to expedite a return journey if radiation, fuel cell problems, or any number of other hazards presented themselves.
In this abort mode, performable up to T+25 hours post-TLI, the CSM or LM engines would be used to null out the majority of the spacecraft's velocity, and allow it to fall back to the Earth. After T+25 hours, the spacecraft would boost itself towards the moon, performing a high speed free-return before reentering the atmosphere. Because of these two abort modes, if any emergency happened on the way to the moon NASA had a small, but usable window of time to save the crew. Apollo 5 splashed down safely, less than a day after liftoff.