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applications program

Apollo Applications Program

The Apollo Applications Program (AAP) was established by NASA headquarters in 1968 to develop science-based manned space missions using surplus material from the Apollo program. AAP was the ultimate development of a number of official and unofficial Apollo follow-on projects studied at various NASA labs.

Origins

Initially the AAP office in Washington was an off-shoot of the Apollo "X" bureau, also known as the "Apollo Extension Series". AES was developing technology concepts for mission proposals based on the Saturn IB and Saturn V boosters. These included a manned lunar base, an earth-orbiting space station, the so-called Grand Tour of the Outer Solar System, and the original "Voyager program" of Mars Lander probes.

AES (Apollo Extension Series) Lunar Base

The Apollo lunar base proposal saw an unmanned Saturn V used to land a shelter based on the Apollo Command/Service Module (CSM) on the moon. A second Saturn V would carry a three-man crew and a modified CSM and Apollo Lunar Module (LM) to the moon. The two-man excursion team would have a surface stay time of nearly 200 days and use of an advanced lunar rover and a lunar flier as well as logistics vehicles to construct a larger shelter. The isolation of the CSM pilot was a concern for mission planners, so proposals that it would be a three-man landing team or that the CSM would rendezvous with an orbiting module were considered.

Evolution

The following phases were considered:

  • Phase 1: 1969-1971: This "Apollo Phase" commenced with the first lunar landing and continued for four missions, or until sufficient experience had been achieved to allow the next phase to commence. As actually flown by NASA, these missions corresponded to Apollo 11 to Apollo 14.
  • Phase 2: 1972 to 1973: This Lunar Exploration Phase would commence about two years after Apollo and consisted of four flights of the Extended Lunar Module (ELM), a modification of basic Apollo Lunar Module hardware. ELM missions extended lunar stay time to 3 or 4 days with landed payloads approaching 450 kg. This scenario corresponded to Apollo 15 to Apollo 17 as flown.
  • Phase 3: 1974: A single Lunar Orbital Survey Mission was indicated after the Lunar Surface Exploration phase and would be the end of the initial buy of Apollo spacecraft. This 28-day lunar polar orbit mission would be flown after the Apollo's and ELM's, in order to have several "ground-truth" sites.
  • Phase 4: 1975-1976: This Lunar Surface Rendezvous and Exploration Phase nominally consisted of two dual-launch missions. A Lunar Payload Module (LPM - essentially the LM Truck of earlier studies) would be delivered by an unmanned cargo carrier to the surface and provide a rendezvous target for a manned ELM that would arrive up to 3 months later.

Associated vehicles

The Apollo LM Taxi was essentially the basic Apollo LM modified for extended lunar surface stays. This was expected to be the workhorse of both Apollo Applications Extended Lunar Surface Missions beginning in 1970 and to larger Lunar Exploration System for Apollo in the mid- to late- 1970's.

The Apollo LM Shelter was essentially an Apollo LM with ascent stage engine and fuel tanks removed and replaced with consumables and scientific equipment for 14 days' extended lunar exploration.

The MOBEV F2B was a multi-man surface-to-surface flying vehicle.

LESA (Lunar Exploration System for Apollo) Lunar Base

The basic Apollo hardware would evolve into AES (Apollo Extension Systems), followed by ALSS (Apollo Logistics Support System), and then LESA (Lunar Exploration System for Apollo). The end result would be ever-expanding permanent stations on the moon.

LESA (Lunar Exploration System for Apollo) represented the last lunar base concept studied by NASA prior to the cancellation of further Saturn V production. LESA would use a new Lunar Landing Vehicle to land payloads on the lunar surface and extended CSM and LM Taxi hardware derived from the basic Apollo program would allow crews to be rotated to the ever-expanding, and eventually permanent, lunar base. A nuclear reactor would provide power.

Phases:

  • 2 men/2 days - Apollo
  • 2 men/14 days - AES - LEM Shelter (2050 kg surface payload - LEM Shelter)
  • 2 men/14 to 30 days - ALSS with shelter or MOLAB (4100 kg surface payload)
  • 3 men/90 days - LESA I (10,500 kg surface payload)
  • 3 men/90 days - LESA I + MOLAB (12,500 kg surface payload)
  • 6 men/180 days - LESA II with shelter and extended-range roving vehicle (25,000 kg surface payload)

Lunar Escape Systems

To support longer stays on the Moon, NASA also studied a number of simple Lunar Escape Systems as a means of returning two astronauts from the lunar surface to an orbiting CSM if the Lunar Module ascent-stage engine failed to ignite.

Manned Venus Flyby

Another plan for Apollo-based extended-duration manned spaceflight would use a Saturn V to send three men on a Manned Venus Flyby, using the Saturn S-IVB stage as a 'wet workshop'. First the S-IVB would boost itself and the Apollo CSM on a trajectory that would pass by Venus and return to Earth, then any remaining fuel would be vented to space, after which the astronauts would live in the empty fuel tanks until they separated from the S-IVB shortly before reentry on their return to Earth.

Development

When procurement of Saturn Vs other than those required for the lunar landing was stopped in 1968, focus shifted to AAP. Aside from attempting to show that Apollo presented value for money, NASA and the main contractors of Boeing, Grumman, North American Aviation and Rockwell also hoped to put off the inevitable scaling down of staff and facilities following the completion of the first Moon landing.

Three AAP proposals were selected for development:

The Apollo Telescope Mission would be an Earth-orbiting mission for solar observation. The telescope would be based on a modified Lunar Module ascent stage, and launched using a S-IVB. The telescope would be docked to a CSM with a three-man crew. Solar panels on the telescope would provide additional power, allowing an extended mission of 21-28 days. The telescope module would include a pressurized compartment providing additional living and workspace for the crew.

The Apollo Manned Survey Mission proposed an Earth-observation science module also based on the LM ascent stage, and would also have been launched using a S-IVB vehicle into a high-inclination orbit. It was also proposed that a surplus Saturn V would launch a manned lunar survey mission to establish suitable sites for later manned landings.

The wet workshop space station concept provided for a low-budget Earth orbiting station. The original plan, as proposed by Wernher von Braun, used the S-II stage as the primary structure of the station, with the area normally filled by the S-IVB stage replaced with an equipment carrier. These plans were modified to use the S-IVB when Saturn V production ended with just enough boosters for the lunar missions alone.

In the meantime several of the Earth-orbit "checkout" missions for Apollo had been canceled, leaving a number of Saturn IB's unused. The plans were changed to use the S-IVB stage, used on both rockets, as the primary station structure. A modified S-IVB would be launched into orbit, the second stage carrying a docking module and large solar panels in the area normally carrying the LM. A CSM would then be able to dock with the second stage and enter the now-empty fuel tanks. It was also suggested that the Apollo Telescope and Survey Mission modules might be docked to the Wet Workshop to create a modular space station.

Skylab

Originally, AAP missions would alternate with Apollo lunar missions, starting in 1969. However when NASA's 1969 budget was cut, focus was shifted to the Skylab space station proposal, which managed to accommodate the equipment already specified for some of the AAP missions. Specifically, Skylab included the Apollo Telescope Mission (renamed the Apollo Telescope Mount) attached to the docking station used by the CSMs. Since the Saturn V stack placed the S-IVB in orbit without it needing to fire on its own, the extra lift capacity of the stage was not needed and it could be launched "dry". This allowed the interior space to be better fitted out, although many design concepts from the Wet Workshop, notably the open flooring that allowed fuel to flow through it, were kept in Skylab.

The concept of launching one of the "Spare" unused Skylabs into lunar orbit was briefly discussed around the same time, but no justification could be found for it, so the project was abandoned early on.

References

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