05 July 2015

"Assuming That Everything Goes Perfectly Well in the Apollo Program. . ." (1967)

The AS-204 Saturn IB launch vehicle - the rocket originally intended to launch Apollo 1, the first piloted Apollo mission in February 1967 - configured to launch Apollo 5, the first unmanned Lunar Module test flight, in January 1968. Image credit: NASA
Usually in this blog I devote my attention to technical documents and their historical context. I do not normally focus on press conference transcripts. The 26 January 1967 NASA Headquarters press conference led by George Mueller, Associate Administrator for Manned Space Flight, and Charles Mathews, Apollo Applications Program (AAP) Director, is, however, significant enough to be given its own post.

AAP's main stated aim was to gather scientific knowledge in space for the benefit of people on Earth. The program mainly sought to modify Apollo spacecraft and Saturn rockets to do things other than reach for the moon, but also aimed to enhance NASA's lunar exploration capability. The Command and Service Module (CSM) spacecraft and the two-stage Saturn IB rocket were envisioned as the AAP workhorse vehicles, though the Lunar Module (LM) and the giant Saturn V rocket would also play important roles.

Though Mueller did not say as much, AAP's conceptual roots went back nearly to the Apollo Program’s birth. In April 1963, for example, less than two years after President John F. Kennedy made landing a man on the moon a national priority, NASA's Manned Spacecraft Center (MSC) in Houston, Texas, contracted with CSM spacecraft prime contractor North American Aviation (NAA) to study how the spacecraft might be converted into a six-man transport for Earth-orbital space station crew rotation and logistics resupply.

The AAP press conference followed NASA's Fiscal Year (FY) 1968 budget briefing on 23 January, during which NASA Administrator James Webb and Deputy Administrator Robert Seamans told reporters that President Lyndon Baines Johnson had authorized NASA to seek a total of $454.7 million for AAP in FY 1968. Despite the fact that it had existed for nearly two years as a formal program, most reporters present at the budget briefing knew little of AAP, so they prevailed upon the space agency to provide more information. The 26 January press conference was NASA's response.

Among the few space-savvy members of the press corps, the Johnson Administration's evident enthusiasm for AAP piqued interest. The White House had, after all, sought $270 million for AAP in FY 1967, only to see Congress appropriate just $80 million. Leaders in Congress had cited the escalating cost of war in Indochina when they slashed the President's FY 1967 AAP request. That President Johnson would expend political capital on the program for a second year in a row – and ask for almost double the sum he had been refused the previous year – indicated strong Executive Branch support for AAP.

When reporters arrived at NASA Headquarters for the press conference late in the afternoon on 26 January, they found on their seats a 10-page packet of detailed information on AAP. In this post, I have fleshed out some of Mueller's generalizations by referring to the AAP press packet.

Mueller told the assembled reporters that the time was ripe for starting AAP. "By the end of this year," he declared, "we will have flown men on at least two of the Saturn V launch vehicles, and we will have tested both the [LM] and the [CSM]." He did not need to tell the reporters that the first piloted flight of the Apollo Program, designated Apollo 1 or AS-204, was scheduled for launch on 21 February, a little more than three weeks after the AAP press conference. Apollo 1 was planned as a 14-day Earth-orbital test of the Apollo CSM launched on a Saturn IB rocket.

June 1966: Artist concept of Apollo Program launch vehicles and spacecraft. The Saturn V (left) included the S-IC first stage, the S-II second stage, the S-IVB third stage, and the Apollo spacecraft depicted in the center of the illustration. The "Uprated Saturn I" (right) was by January 1967 renamed the Saturn IB, which included the S-IB first stage, the S-IVB second stage, and the Apollo spacecraft. The Saturn V and Saturn IB S-IVB stages were essentially identical. The Command Module and Service Module together formed the Command and Service Module (CSM) spacecraft. The Lunar Module (LM) rode into space inside the tapered Spacecraft Launch Adapter (SLA) shroud (not labeled), which could also fly empty or with payloads other than the LM inside. Image credit: NASA
Mueller reminded his audience that NASA had ordered 12 Saturn IB rockets and 15 Saturn Vs for the Apollo lunar program. He expected that fewer than that would be needed to reach the goal of a man on the moon before the end of the 1960s decade. It was from the surplus that the two-stage Saturn IB rockets needed for the first AAP missions would be drawn. As soon as the Apollo Program was finished with Earth-orbital test missions launched on Saturn IBs, AAP missions could begin. In fact, Mueller saw no reason why AAP Saturn IB-launched Earth-orbital missions and Apollo Saturn V-launched moon missions could not occur simultaneously.

"Assuming that everything goes perfectly well in the Apollo Program," Mueller told the reporters, by late 1968 or early 1969 NASA could have in 275-nautical-mile-high Earth orbit "an embryonic space station or the first step toward a space station. . .with the capability of reuse and resupply." The station might operate for more than three years before Earth's thin upper atmosphere dragged it down from orbit.

NASA did not have firm plans for staffing the AAP station throughout its time in orbit, Mueller explained. He declared, however, that the four missions required to establish the planned initial AAP capability constituted "a program that is firm, and is proceeding."

The first of the four "firm" missions, designated AAP-1, would begin with the launch of a Saturn IB rocket with a piloted CSM on top. Upon attaining orbit, the three-man crew would turn their spacecraft end-for-end and dock with a prototype Mapping & Survey System (M & SS) module stored in the Saturn Launch Adapter (SLA), the segmented, streamlined shroud that during ascent to orbit linked the bottom of the CSM with the top of the Saturn IB's S-IVB second stage. During an independent flight period lasting about a week, the AAP-1 crew would use the M & SS to record data on the oceans, landmasses, and atmosphere for the benefit of people on Earth.

Four or five days after the AAP-1 astronauts began their program of Earth observations, NASA would launch the unmanned AAP-2 Saturn IB with an SLA with a conical aerodynamic shroud on top in place of a CSM. The rocket would resemble the one in the image at the top of this post. The SLA and conical shroud would cover an airlock and a docking adapter with five ports. Charles Mathews, who had headed up MSC's Gemini Program Office before becoming NASA Headquarters AAP Director, added that the airlock would include a Gemini spacecraft hatch for exiting the station to perform spacewalks.

The AAP-2 S-IVB stage would inject itself, the SLA, the airlock, and the docking adapter into its 275-nautical-mile-high operational orbit using its single J-2 engine, then flight controllers would command the spent stage to "passivate" itself. Their command would open vents in the S-IVB stage tanks and engine to exhaust into space all liquid hydrogen fuel and liquid oxygen oxidizer remaining on board. In answer to a reporter's request for more detail, Mueller added that small spherical helium tanks bolted to the lining of the 21-foot-diameter, 10,000-cubic-foot liquid hydrogen tank would also be vented – the inert helium was on board to pressurize the liquid hydrogen tank, forcing propellants into the J-2 engine – and that the stage would automatically "disconnect the various electrical things that might cause a problem."

The S-IVB stage would also deploy electricity-generating solar arrays from two of its four folded-back SLA shroud segments and a meteoroid shield that would stand several inches off the skin of the two-thirds of the S-IVB stage that contained the liquid hydrogen tank. The shield, a thin layer of metal, would break up any micrometeoroids that might hit it, preventing them from penetrating the stage skin and liquid hydrogen tank within.

Artist concept of AAP-2 spent-stage station with AAP-1 Apollo CSM docked at axial port and AAP-1 Mapping & Survey System docked at radial port. Image credit: NASA
The AAP-1 CSM would rendezvous with the AAP-2 spent-stage station and dock the M & SS with one of the docking adapter's four radial ("side") ports. It would then undock from the M & SS and dock with the docking adapter's axial ("front") docking port.

The AAP-1 astronauts would enter the 65-inch-diameter, 1000-cubic-foot docking module, where would be packed furnishings for outfitting the interior of the liquid hydrogen tank. Before they could deploy the furnishings (a process that would need three or four days), they would use controls in the airlock to close the vents in the liquid hydrogen tank and fill it with a mixture of three-fifths oxygen and two-fifths nitrogen at five pounds per square inch of pressure. Gaseous oxygen and nitrogen for pressurizing the liquid hydrogen tank would reach orbit in tanks bolted to the outside of the airlock module.

Mueller likened putting the furnishings packed in the docking adapter into the liquid hydrogen tank to "building a ship in a bottle." The astronauts would open a 43-inch-diameter hatch leading into the tank. The tank's interior would be modified during manufacture to include tie-downs and attachment points for installation of galley, hygiene, exercise, sleep, and experiment equipment, as well as lights and ventilation ducts and fans.

Though illustrations he displayed during the press conference showed pre-installed walls and grillwork floors, Mueller told a reporter that "I don't know that we will want to put additional things [besides the tie-downs and attachment points] inside" the liquid hydrogen tank. If the decision were taken to minimize tank modifications, then the astronauts would string fabric floors and walls within the tank, he explained. A "rope" running the length of the tank would aid mobility. He added that he was "sure that we will use liberal amounts of velcro."

Mueller was quick to note that few experiments had been officially manifested for any AAP flight; some of the $454.7 million the White House had requested for AAP in FY 1968 would go toward new experiment development. There were, for example, no biology experiments yet approved, though seven medical experiments were on track for flight. NASA also expected to include Defense Department experiments that would focus on "how to work in space" and test "jet shoes." Mueller likened them to "roller skates with gas jets on them."

He explained that experiment packages scheduled specifically for the AAP-1/AAP-2 mission would, among other things, aim to "find out what happens to the flammability of materials, how they actually burn when you have a combination of oxygen and nitrogen and. . .zero gravity." In addition, the astronauts would continue to use the M & SS for Earth observations, and would test a combination sleep/space suit-donning station.

The AAP-1 astronauts' stay on board the AAP-2 spent-stage station was scheduled to last for about 28 days, or twice as long as Gemini 7 (4-18 December 1965), which at the time of the 26 January press conference was the world record-holder for piloted space mission duration. As the AAP-1/AAP-2 mission drew to a close, the crew would shut off experiments and station systems and undock in their CSM. They would then ignite the CSM's Service Propulsion System main engine to deorbit, cast off the Service Module (SM), reenter the atmosphere, deploy parachutes, and splash down at sea in the conical Command Module (CM).

Between three and six months later – no later than mid-1969 – NASA would launch the AAP-3 mission to the AAP-2 station. A piloted CSM loaded up with supplies would ride a Saturn IB to orbit. Mueller told his audience that he favored putting supplies in a special module that would ride to orbit in the SLA, much as had the M & SS; however, the illustrations he showed to the press did not depict such a module.

The LM-derived AAP-4 Apollo Telescope Mount maneuvers to a docking at the AAP-2 radial port opposite the AAP-1 Mapping & Survey System while the AAP-3 CSM stands by. Image credit: NASA/David S.F. Portree
One day after the AAP-3 launch, NASA would launch the unmanned AAP-4 Saturn IB bearing beneath its SLA and conical shroud the Apollo Telescope Mount (ATM). The ATM was envisioned as a modified Apollo LM with solar arrays and solar observatory instruments in place of descent and ascent engines and landing legs.

The AAP-3 CSM would dock with the ATM, withdraw it from the top of the AAP-4 Saturn IB S-IVB stage, and transport it to the AAP-2 station. An astronaut would then board the ATM, undock from the CSM, and, using the ascent stage attitude control thruster quads for propulsion, pilot it to a docking at one of the station's docking module radial ports. The CSM would stand by until ATM docking was successfully completed, then would dock at the station's axial port. The ATM would then deploy solar arrays, which would provide it with electricity.

Mueller explained that the ATM was scheduled for launch in 1969 because the Sun's 11-year cycle of activity would peak in that year. The ATM would, he told the reporters, carry "the most comprehensive array of instruments that has ever been assembled for observing the Sun." An astronaut at the ATM control panels in the modified LM ascent stage would keep a constant vigil on the Sun, and would rapidly direct the instruments toward interesting phenomena as they appeared. The ATM might operate at the end of a tether attached to the docking adapter to minimize the effects on the quality of the data it collected of astronaut movements inside the spent-stage station.

Of course, the chief benefit of the ATM would be scientifically important but essentially abstract knowledge about the structure and behavior of the Sun. AAP was, however, meant to bring benefits of space to people on Earth, so Mueller opined that a better understanding of the Sun would "have marked benefits on our own understanding of how to generate and control energy here on Earth."

The AAP-3 crew would seek to double the AAP-1 crew's stay-time in space, setting a new record for space endurance of 56 days. In addition to operating the ATM, they would continue many of the experiments begun by the AAP-1 astronauts.

Mueller then described APP payloads, missions, and capabilities that would begin to be developed if Congress voted to provide the funding for AAP that the White House had requested for FY 1968. In answer to a reporter's question, he explained that the AAP-2 spent-stage station would remain at the center of the program's Earth-orbital activity "until something fails," at which time NASA would launch a fresh spent-stage station.

Reusability would be a hallmark of AAP, Mueller explained. The term “reusability” had at least two meanings in the program. On the one hand, it meant that for as long as they could function, the AAP stations would host new crews and instrument payloads. On the other, it meant that certain hardware elements – in particular the Apollo CM – would be redesigned for refurbishment and multiple flights. Both approaches to reusability aimed to cut costs.

Mueller called the Apollo CM "one of the most expensive elements of the space vehicle." He described for reporters an uprated CM for later AAP flights that would touch down on land, not splash down at sea. "Since we don't dunk it in salt water at the end of the flight," he explained, "we don't then have quite the same corrosion problem. . .that we do with those [CM]s that are water landed."

Landing the CM on solid ground would, Mueller noted, also help NASA to double its normal three-person crew complement. Steerable parachutes and view screens would enable the crew to pilot their CM to a predetermined landing zone; then, five or 10 feet above the ground, retrorockets behind the heat shield would ignite, slowing the CM to a touchdown speed of three or four feet per second. Normal Apollo splashdown speed was, Mueller explained, 10 or 20 feet per second; reducing that velocity meant that shock-absorbing struts supporting the CM crew couches would not stroke very much to absorb landing shock, so would not need as much empty space behind them as in the baseline CM. This would enable NAA contractor engineers to install a new row of three couches behind the existing three Apollo CM couches.

Mueller then described three "payload packages" that might be added to AAP stations if funding allowed. AAP-A was a "Meteorology Payload Package" with 14 experiments which would, it was hoped, reach orbit on a Saturn IB in mid-1969. AAP-B, the "Earth Resources Payload Package" with 12 experiments on board, would follow in mid-1970. By then, Mueller told his audience, a three-man crew might live on board an AAP station for an entire year.

The "Manned Photographic Telescope," an ultraviolet telescope with a meter-wide aperture, might be docked to an AAP station in a high-Earth orbit, Mueller explained, in order to permit observation periods longer than were possible in the AAP-2 station's low orbit. A station high above Earth would need more time to complete an orbit, thus potentially permitting continuous observation of an astronomical target over the space of hours. The AAP-2 station, by contrast, would circle Earth in about 90 minutes, enabling less than 45 minutes of observation before the target dropped out of sight below Earth's horizon.

Placing an AAP station in high-Earth orbit would demand a more powerful launcher than the Saturn IB; specifically, the Saturn V. The S-IVB stage that formed the second stage of the Saturn IB served also as the Saturn V third stage, so could be put to use as an AAP spent-stage station in high-Earth orbit with only modest modifications.

1966 NASA artist concept of the baseline Apollo Lunar Module. 
The Manned Photographic Telescope was scheduled for launch in 1971-1972, so there was a good chance that other Saturn V-launched AAP missions might precede it. AAP planners expected that, after a series of Early Apollo lunar landing missions starting around the end of 1968, Saturn V-launched AAP lunar missions would take over. Early Apollo missions would spend up to 36 hours on the lunar surface and support 1000-foot moonwalks; AAP lunar missions might last 14 days and support traverses up to 15 miles from base camp.

Mueller expected that each AAP lunar mission would need two Saturn Vs; one to launch a CSM/LM Shelter combination and one to launch a CSM/LM Taxi combination. The Shelter, which would land at the candidate landing site without a crew, would house the two astronauts who arrived later in the Taxi.

The LM Taxi would be designed to park on the lunar surface, its major systems shut down, for 14 days, then "wake up" so that the astronauts could lift off in its Ascent Stage to rejoin the CSM Pilot in lunar orbit. Outwardly the Taxi would resemble the Apollo LM.

The LM Shelter, on the other hand, would need many very obvious modifications. Some concepts had all descent systems in the Ascent Stage moved to the Descent Stage and the Ascent Stage replaced entirely with a purpose-built habitat module; others only stripped out ascent systems and propellants and left the Ascent Stage otherwise intact. Regardless of its design, the LM Shelter would require modifications to enable an automated or remote-controlled landing and a long quiescent stay on the moon ahead of LM Taxi arrival.

The LM Shelter would also carry attached to its sides a heavy load of exploration equipment. This might include a "jeep" for surface mobility, a drill for boring 300-foot-deep holes, an instrumented "subsurface probe" for lowering down the bore hole, an astronaut-carried "survey system" for stereo imaging and precise post-flight location of sampling sites and traverse routes, and an elaborate suite of automated science instruments that would continue to operate long after the AAP lunar mission crew returned to Earth.

The AAP lunar landing missions, which would occur about a year apart, might be preceded by one or more AAP lunar-orbital mapping missions. These would see a CSM with an M & SS docked to its nose operate in lunar polar orbit for at least 14 days. The astronauts on board would map the entire moon in much greater detail than could the automated Lunar Orbiter series, which was on-going at the time of the AAP press conference. This would enable improved landing site selection and traverse planning for the AAP lunar missions. The advanced lunar missions would probably rely on Saturn V rockets built specifically for AAP; that is, not part of the original 15-rocket "buy" for the Apollo moon program.

Both Mueller and the assembled reporters seemed to downplay AAP lunar missions, as if all realized that they were the part of AAP least likely to receive funding from Congress. Though they would yield fascinating data, they ran against the grain of AAP. The people on Earth who would benefit most from the AAP lunar missions were, it seemed, the people hired to build the lunar mission hardware. In general, the reporters assembled for the 26 January press conference looked with suspicion upon aspects of AAP that seemed to them mainly to mean continued pork for certain states and congressional districts.

Interestingly, it was Charles Mathews, former MSC Gemini director, who was most successful in explaining the potential of AAP in NASA's post-Apollo program. He told the reporters that "between Mercury and Apollo. . .we had a program called Gemini, where we learned to do many of the things. . .that we are going to [do] in [AAP] and in the Apollo Program." Mathews argued that AAP could serve the next big NASA program, whatever it might be, as Gemini had served Apollo. "[Before] we go on to planetary operations or space station operations," he said, "we need to develop experience in these long-duration operations. . .So [AAP] is a rather logical approach."

Left to right: Apollo 1 crewmembers Ed White, Gus Grissom, and Roger Chaffee pose with a model of the Apollo CM. Image credit: NASA
The 26 January press conference drew to a close at 5:30 pm Eastern time. Twenty-four hours later, at Cape Kennedy, Florida, astronaut Gus Grissom, commander of the Apollo 1 mission, was growing frustrated. He had been strapped on his back inside CSM-012 on the pad at Launch Complex 34 for several hours with his shipmates Roger Chaffee, a spaceflight rookie, and Ed White, the first American to walk in space. Grissom had for at least a year worried that CSM-012 suffered from more than its share of technical faults. The pre-flight test on 27 January encountered one glitch after another.

One problem was "ratty" communications – crackly static and voice drop-outs – between flight test control and the spacecraft. Controllers put the test countdown on hold while they tried to correct the problem. Grissom raised his voice above the static: "How are we going to get to the moon if we can't talk between two or three buildings?"

At 6:31 pm, flight controllers heard the word "fire" spoken over their crackling headsets. A spark, possibly the result of faulty wiring insulation, had set alight materials in the CM cabin that had not been adequately tested for fire resistance in its pure oxygen atmosphere. These included liberal quantities of velcro. Almost before they could react, Grissom and his crew were asphyxiated as flames burned up their air hoses and consumed the oxygen inside their capsule. Heat and pressure built up inside the CM until its pressure hull cracked, spewing acrid smoke into the enclosed service area surrounding the capsule.

The pad crew suffered smoke inhalation and burns as they fought to open the CM's balky, poorly designed inward-opening hatch. They gave no thought, however, to abandoning their efforts to save Grissom, Chaffee, and White.

Through the small hatch window they could see only dense smoke. When they finally succeeded in pushing back the hatch about five minutes after the fire began, the terrible truth was made plain. The United States had suffered the world's first spaceflight fatalities, and they had happened on the launch pad, during what was supposed to be a routine pre-flight practice run, not during flight through space or on the moon.

NASA and the Congress quickly went to work to investigate the fire. The NASA-appointed AS-204 Review Board displayed commendable impartiality; it found many hardware and procedural faults throughout the Apollo Program and evidence of rocky relations between CSM contractor NAA and NASA's Office of Manned Space Flight spanning years. NASA's allies in Congress became angry because the space agency had not shared with them its concerns regarding NAA workmanship.

NASA officials testify before Congress in the aftermath of the Apollo 1 fire. Left to right: Deputy Administrator Robert Seamans; Administrator James Webb; Associate Administrator for Manned Space Flight George Mueller; and Apollo Program director Samuel Phillips. Image credit; NASA
Congress could not "punish" NASA by cutting the Apollo budget; to do so would have imperiled achievement of the national goal of a man on the moon by 1970. It could, however, express its disquiet by attacking AAP. For a time in the summer of 1967, it appeared that AAP's FY 1968 budget might be cut to $300 million, a figure which NASA officials stated would permit a reasonable amount of progress during the year that followed. In the end, however, Congress slashed the FY 1968 AAP budget to only $122 million.

Some expected President Lyndon Baines Johnson to fight for AAP; however, he instead acquiesced to the cuts, declaring that "some hard choices must be made between the necessary and the desirable. . .We dare not eliminate the necessary. Our task is to pare the desirable." It appeared to some that NASA had lost its future.

Appearances could be deceiving, however. In a late November 1967 presentation to the American Astronautical Society's Astronautics International Symposium in New York City - following close on the heels of Apollo 4, the successful first unmanned test of the Saturn V rocket (11 November 1967) - Charles Mathews outlined an AAP program only a little different from the one he and Mueller described the day before the fire. In fact, it included two new missions: AAP-1A, a CSM/M & SS mission without a spent-stage workshop that would take over AAP-1's Earth observations and ease NASA into AAP-1/AAP-2, and AAP-5, which would deliver an unspecified payload package to the first spent-stage station and extend astronaut orbital stay-time past 56 days.

In the new plan, AAP-1 and AAP-2 traded places; that is, the spent-stage workshop would reach space first and be designated AAP-1. Mathews also gave brief mention to two undesignated missions: these would see launch of a piloted CSM plus an unspecified payload package and a second spent-stage AAP station.

It soon became clear that AAP retained high-level support, for in mid-January 1969, the Johnson White House requested $439 million for the program in FY 1969. This was about half the budget NASA had planned for AAP in FY 1969 before the fire, but was deemed sufficient to move forward with the program.

Events on the other side of the world intervened, however. The Tet Offensive, which saw Viet Cong and North Vietnamese forces simultaneously attack U.S. and South Vietnamese bases, was the largest campaign of the Vietnam War. It began on 30 January 1968, on the eve of Tet, the Lunar New Year, and continued through much of February. Tet put U.S. forces on the defensive and dramatically increased the human and financial cost of waging war in Indochina.

AAP had been on shaky ground with Congress even before the Tet escalation. By the time it completed its deliberations, the Legislative Branch cut Johnson's FY 1969 AAP request by nearly half to $277 million. Other cuts in NASA funding caused NASA Administrator James Webb to put Saturn rocket production on hold. AAP entered a kind of limbo: capable of moving forward with near-term development, but with little prospect of accomplishing the more ambitious missions that gave near-term development a purpose.

It is interesting to speculate how AAP might have unfolded had the Apollo 1 fire not occurred. It seems likely that, had NAA delivered a better-quality CSM-012 spacecraft, a successful Apollo 1 mission would have increased (or at least not decreased) support for AAP. The program might then have received adequate funding in FY 1968, permitting it to become better established.

The Tet Offensive would have occurred as it did in our timeline, so Congress would probably not have granted the Johnson Administration's full FY 1969 AAP funding request. Because the program would have become better established during FY 1968, however, the cuts might not have been so deep.

The LM probably would have been delayed, as it was in our timeline, leading perhaps to calls for NASA to focus its energies on Apollo, not AAP. Alternately, a successful Apollo 1 mission in February 1967 followed by the successful Apollo 4 Saturn V test might have made the LM delay seem a little less important.

It appears possible that, had no Apollo 1 fire taken place, NASA might have launched an AAP spent-stage station by late 1968. When an astronaut – perhaps Apollo 1 commander Gus Grissom – became the first man to set foot on the moon late in 1968 or early in 1969, three astronauts on board the AAP station in low-Earth orbit might have gathered around a flickering small monitor to watch the historic event.


Apollo Applications Briefing, NASA News, NASA Headquarters, 26 January 1967

Apollo Applications – A Progress Report, Charles Mathews; presentation at the American Astronautical Society Astronautics International Symposium, 27-29 November 1969

Living and Working in Space: A History of Skylab, NASA SP-4298, W. David Compton and Charles Benson, NASA, 1983

“White House Stand Blocks NASA Budget Restoration,” Aviation Week & Space Technology, 28 August 1967, p. 32

More Information

Space Station Resupply: The 1963 Plan to Turn the Apollo Spacecraft Into a Space Freighter

A Bridge from Skylab to Station/Shuttle: Interim Space Station Program (1971)

An Alternate Station/Shuttle Evolution: The Spirit of '76 (1970)

A Forgotten Rocket: The Saturn IB


  1. Thank you for this, David! Skylab in 1969... a dizzying prospect.

  2. Iroman-1 https://en.wikipedia.org/wiki/Marooned_%28film%29
    And if the Apollo 13 service module was assigned to the Apollo of the first AAP crew direct to the station?
    The service module explode and the three astronauts are marooned in orbit.
    But maybe another Apollo AAP is on the ramp,and NASA tries a rescue mission....

  3. If the incident happens on AAP-3 in the outward voyage,the Apollo crew have the ATM for extra oxygen and energy,while NASA prepares AAP-4 for the rescue.

  4. Carmelo:

    The AAP CSM would have had a design different from that of the Apollo CSM. Certainly they'd have stripped out the fuel cells and replaced them with batteries and water tanks; tanks inside the SM would have been modified, too. Probably the ATM would have kept the batteries in the SM charged through a fixture in the CM docking unit. One can imagine many things going wrong - Skylab 3 had thruster leaks which caused NASA to roll the rescue CSM to the launch pad - but I don't think that a replica of the Apollo 13 explosion would have been likely.

    Another thing one might consider - the ATM design had LM thruster quads for separating from the CSM and steering to a docking at one of the workshop radial ports. Even if the SM thruster quad had been knocked out, those would have been available. I suspect that they wouldn't have been capable of deorbiting the CSM or even just the CM alone, but they might have.

    So, some other options to consider.


  5. Interesting article on AAP history - a fascinating program which unfortunately doesn't get much mention.

    I've a question about double taxi/shelter AAP lunar missions, the answer to which I couldn't find in any book/document mentioning them: all sources I've seen refer to these missions duration as either "up to", or more often exactly 14 days.

    But after LM-Taxi had landed, the CSM orbit plane would drift by about 13 degrees/day - until the difference will reach its maximum of 180 degree after 14 days, making it impossible for LM to reach CSM - unless it is on a polar orbit? I believe you've wrote of a proposal to use polar orbit for LM-Shelter delivery flights, but I've never heard of such suggestions for LM-Taxi missions (in fact, wouldn't that eliminate the need for I missions which were proposed at the same time?).

    So how could LM-Taxi rendezvous with CSM after 14 day lunar stay? Had I missed something, or were these missions restricted to a narrow band near equator so that CSM could change inclination before rendezvous?


  6. BC -

    The Dual Apollo missions would probably never have flown; NASA was moving toward an Extended Lunar Module (ELM) or Augmented Lunar Module (ALM) concept. Partly this was because of funding cuts in AAP. The ELM was basically the J-class LM, while the ALM would have been capable of a seven-day stay on the moon. ALM might have been coupled with a stripped-down Descent Stage for cargo delivery, but would not have had to stay healthy on the moon after landing the way the LM Shelter would have. There was discussion of building the cargo lander so it could reach the moon on a Titan III by itself - that is, without a CSM and crew - but that didn't go very far because AAP lunar missions went by the boards.

    I think it helps to imagine the moon revolving under the CSM. The CSM orbital plane would in fact remain locked relative to everything except the moon. So, after 14 days, the CSM would be passing over the landing site again, but coming from the opposite direction. After 28 days, it would be passing over the landing site coming from its original orbital direction. So, after 14 days, no plane change would be necessary. Mascons and venting might have tweaked the orbit a bit, but not enough to worry much about.

    What about the 3.5-day ELM stays and the 7-day ALM stays? What about an abort from the surface in the middle of a 14-day stay? The CSM/LM Ascent Stage combo had enough delta-V to accommodate some degree of plane change - certainly enough for the J-class missions, which stayed for ~3.5 days at sites up to about 25 deg from the equator. Probably not enough to accommodate a 7-day stay, so the CSM would have had to be beefed up.

    One study proposed nixing the SIM Bay to accommodate more propellants. Of course, that would cut into the science in a big way and leave the CSM Pilot with very little to do. Other studies assumed a SIM Bay and more propellants - not sure how they managed that, unless they assumed some mass savings in the Taxi.

    That might have been possible - the Taxi would not have needed to support its crew for more than a few hours total and might have carried no science payload.

    The necessary plane change would have been harder to do with the ALM. One idea I've seen mentioned - but not in much detail - would be for the CSM to rendezvous with a recon sat in lunar orbit, dock with it, and use its instruments. So, there'd be no need for a SIM Bay. (However, if the recon sat was a functional spacecraft by itself, it wouldn't have needed a CSM around - except perhaps to collect and return its exposed film.)

    The polar-orbiting LM Shelter delivery flights were meant to combine the I-class missions and the Dual Apollo missions. Two reasons: cost savings (no separate I missions) and giving the crew that dropped off the Shelter something to do (they'd do the I mission).

    The long AAP lunar missions were always kind of problematic; as I remarked in this post, even in early 1967, before the really big cuts, the main emphasis was on the Earth-orbital missions. The idea was to get something valuable to people on Earth out of the US space investment. Spin-offs and the like, data on crops, that kind of thing. Kind of depressing, really.

    Hope this helps. Please ask follow-up questions if you want.



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