This page no longer updated from 31 October 2001. Latest version can be found at By Gemini to the Moon!

Gemini Lunar SRS
Gemini Lunar SRS - Exploded view of the Gemini Lunar Surface Rescue Spacecraft. From top to bottom: the Gemini reentry module; the lunar ascent stage; the lunar descent stage; the lunar orbit insertion stage.

Credit: McDonnell Douglas. 23,395 bytes. 183 x 465 pixels.

Right up to the end of the Gemini program, the Gemini spacecraft was considered by its contractor and certain factions within NASA as an alternate means of reaching the moon. The Gemini re-entry capsule, smaller and lighter than that of Apollo, would allow direct launch of a mission to the moon using a single rocket. Alternatively, rendezvous and docking of components launched by two small rockets (Titan 3C's or Saturn IB's) would eliminate the need for development of the Saturn V.

There were several proposals for lunar Gemini, right up to the very end of the program:

August 1961 - Circumlunar Gemini

At its birth Gemini was known as the Mercury Mark II programme. NASA was already committed to the three-man Apollo spacecraft and considered Gemini an interim spacecraft to test rendezvous, docking, and EVA techniques before Apollo was available. But NASA's James Chamberlin and McDonnell Aircraft considered Gemini as a viable competitor to Apollo for the circumlunar and lunar landing missions. Such proposals might be welcomed by the current 'cheaper, better, faster' NASA. But in 1961, as a direct challenge to the Apollo project and Lyndon Johnson's dream of a Southern High Technology Crescent, they were anathema.

The original August 14, 1961 Mercury Mark II program plan went like this:

Mar 1963Gemini 1Unmanned orbital
May 1963 Gemini 2Manned orbital
Jul 1963 Gemini 37-day manned orbital
Sep 1963 Gemini 47-day manned orbital
Nov 1963 Gemini 5Agena docking
Jan 1964 Gemini 614-day primate orbital
Mar 1964 Gemini 7Agena docking
May 1964 Gemini 814-day primate orbital
Jul 1964 Gemini 9Agena docking
Sep 1964 Gemini 10Agena docking
Nov 1964 Gemini 11Centaur docking, boost to high Earth orbit
Jan 1965 Gemini 12Centaur docking, boost to high Earth orbit
Mar 1965 Gemini 13Centaur docking, boost to Lunar flyby
May 1965 Gemini 14Centaur docking, boost to Lunar flyby

The Centaur would be launched atop a Titan II booster. The lunar Gemini spacecraft would have weighed 3,170 kg, an extra 270 kg over the basic rendezvous Gemini. The difference consisted of a backup inertial navigator and additional heat shielding for re-entry at 11 km/sec instead of 8 km/sec. This program was estimated to put an American around the moon for only $ 60 million more than the basic $ 356 million program. An even more aggressive alternative, a nine-flight program, was promised to cost only $ 8.5 million more than the basic program and fly around the moon in May 1964! This first attempt to fly Gemini to the moon was quickly suppressed, and a revision of the plan was issued only a week later, with all mention of lunar flights deleted.

Gemini-CentaurGemini-Centaur - Gemini Docked to Centaur for Circumlunar Flight

Credit: © Mark Wade. 2,766 bytes. 567 x 143 pixels.

September 1961 - Gemini Lunar Landing

But the idea seemed too good to just drop and a month later Chamberlin came up with an even more ambitious plan. He proposed to not just fly around the moon, but to land on it, at a cost 1/20 of that of the Apollo project. The key was the use of the technique of lunar orbit rendezvous and a bare-bones, open cockpit lunar module. This would weigh 4,372 kg in the storable propellant version or 3,284 kg in the cryogenic Lox/LH2 version (calculated propellant loads 3,500 kg and 2,200 kg, respectively). The total mass to be injected into an escape trajectory toward the moon would be no more than 13,000 kg, one fifth of the 68,000 kg planned for the Nova-boosted direct-lunar landing approach favoured at that time. At this mass, instead of Nova, a Saturn C-3 launch vehicle could be used. The flight schedule would have been delayed by a year in order to develop a more capable spacecraft. However by launching every 45 days instead of every 60 days Gemini would still put an American on the moon by January 1966:

Titan 2 Launches
Mar 1964 Gemini 1Unmanned orbital
May 1964 Gemini 2Manned orbital
Jun 1964 Gemini 37-day manned orbital
Aug 1964 Gemini 414-day manned orbital
Sep 1964 Gemini 5Agena docking
Nov 1964 Gemini 6Agena docking
Dec 1964 Gemini 7Agena docking
Feb 1965 Gemini 8Centaur docking, boost to high Earth orbit
Mar 1965 Gemini 9Centaur docking, boost to high Earth orbit
May 1965 Gemini 10LM docking
Jun 1965 Gemini 11LM docking
Jul 1965 Gemini 12LM docking
Sep 1965 Gemini 13Centaur docking, boost to Lunar flyby
Oct 1965 Gemini 14Centaur docking, boost to Lunar flyby
Saturn C-3 Launches
Nov 1965 Gemini 15Manned Lunar orbital
Jan 1966 Gemini 16Manned Lunar landing

Langley 4,372 kg LMLangley 4,372 kg LM - Langley 4,372 kg lunar lander

Credit: © Mark Wade. 993 bytes. 162 x 120 pixels.

The lunar module would have been launched separately by Titan II for the three Earth orbital docking missions. This moon landing project was projected to cost $ 584 million 'plus the cost of two Saturn C-3's'.

Chamberlin was actually the first member of the Space Task Group (STG) to advocate lunar orbit rendezvous (LOR) as a method for reaching the moon. Earlier efforts through 1960 and 1961 by Robert Hoboult and other engineers at Langley to interest STG in the method had been seen as the impractical musings of theorists. Chamberlin and McDonnell Aircraft did not fall in this category. They saw clearly that separating the re-entry and lunar landing functions allowed optimised spacecraft designs for each role, and solved many of the intractable engineering problems the direct-ascent advocates were struggling with.

Chamberlin made one last effort at the end of September to interest STG in including lunar Gemini as part of an "Integrated Apollo Program". This involved the same flight schedule as advocated earlier, but with the cost estimate now firmed up at $ 706 million (including the Saturn boosters!), and the lunar module mass cut to 1,800 kg. NASA brass still rejected the lunar aspects of the plan, but told STG to go ahead with negotiations with McDonnell, Martin, and Lockheed for the spacecraft and boosters. Chamberlin submitted the revised plan without lunar flights on October 27, and this was approved as the basis for project Gemini.

The actual Gemini project as flown was over a year late to the original optimistic plan. This was due to delays in development of both the Titan 2 launch vehicle and the Gemini paraglider landing system. The pivotal 14-day flight actually came in December 1965 versus January 1964 in the first Mercury Mark II proposal and August 1964 in the September 1961 plan.

Langley 1,460 kg LMLangley 1,460 kg LM - Langley 1,460 kg lunar lander

Credit: © Mark Wade. 1,779 bytes. 159 x 193 pixels.

Apr 1964Gemini 1Unmanned booster orbital test; boilerplate spacecraft.
Jan 1965Gemini 2Unmanned suborbital test of spacecraft
Mar 1965Gemini 3 Manned orbital 
Jun 1965Gemini 44-day manned orbital
Aug 1965Gemini 58-day manned orbital
Dec 1965Gemini 714-day manned orbital
Dec 1965Gemini 6Rendezvous with Gemini 7 (Agena target failed to orbit)
Mar 1966Gemini 8 Agena docking
Jun 1966Gemini 9 Agena docking
Jul 1966Gemini 10 Agena docking
Sep 1966Gemini 11 Agena docking
Nov 1966Gemini 12 Agena docking

Gemini Docks with LMGemini Docks with LM - Gemini rendezvous above lunar surface with open cockpit Lunar Module after first lunar landing in 1966

Credit: © Mark Wade. 36,780 bytes. 373 x 288 pixels.

It is possible to estimate when Chamberlin's Gemini moon landing would have actually occurred based on the actual delays to Gemini. It must be considered that the time necessary to develop the Saturn C-3 could not have been much less than that actually taken for the C-5 (the final December 1961 C-3B configuration differed from the C-5 only in the propellant loading in each stage and in having three F-1 engines in the first stage as opposed to five in the C-5). Therefore, with perfect hindsight, if Gemini had been selected in lieu of Apollo, the actual final program would have looked about like this:

Titan 2 Launches
Apr 1964Gemini 1Unmanned booster orbital test; boilerplate spacecraft.
Jan 1965Gemini 2Unmanned suborbital test of spacecraft
Mar 1965Gemini 3 Manned orbital 
Jun 1965Gemini 44-day manned orbital
Aug 1965Gemini 58-day manned orbital
Dec 1965Gemini 714-day manned orbital
Dec 1965Gemini 6Rendezvous with Gemini 7 (Agena target failed to orbit)
Mar 1966Gemini 8 Agena docking
Jun 1966Gemini 9 Agena docking
Aug 1966 Gemini 10Centaur docking, boost to high Earth orbit
Oct 1966 Gemini 11Centaur docking, boost to high Earth orbit
Nov 1966 Gemini 12LM docking
Jan 1967 Gemini 13LM docking
Feb 1967 Gemini 14LM docking
Mar 1967 Gemini 15Centaur docking, boost to Lunar flyby
Apr 1967Gemini 16Centaur docking, boost to Lunar flyby
Saturn C-3 Launches
Aug 1967 Gemini 17Unmanned test of Saturn C-3
Feb 1968 Gemini 18Unmanned Lunar orbital test
Oct 1968 Gemini 19Manned Lunar orbital
Dec 1968 Gemini 20Manned Lunar landing

Gemini-AgenaGemini-Agena - Gemini docked to Agena

Credit: © Mark Wade. 3,073 bytes. 460 x 140 pixels.

So in the end, the first lunar landing would have been moved up by six months at best. There would have been a cost savings, but again analysis of the detailed cost breakdowns for Apollo indicate the savings would have been on the order of 'only' $ 4 billion out of the NASA $ 18 billion project share. So in retrospect it would seem that NASA's management was correct, for the Apollo missions flown were much more capable than a Gemini-based approach would have been.

This was not the end of lunar Gemini. At least three times in the next four years such plans were again actively discussed.

September 1962 - Gemini Lunar Logistics and Rescue Vehicle

In the summer and fall of 1962 NASA headquarters asked Space Technology Laboratories and McDonnell to study use of Gemini as a 'lunar logistics and rescue vehicle'. The eight week study looked at using Gemini to land two men directly onto the lunar surface and identified the design changes required to accomplish this. An estimate was made of the cost of purchasing extra Gemini spacecraft for this purpose. But at that point in time Gemini was in deep financial and schedule problems, and the matter was not pursued further.

March 1964 - Gemini / Saturn IB

In the spring of 1964, with manned Apollo flights using the Saturn I having been cancelled, use of a Saturn I to launch a Gemini around the moon was studied. This could either be flown in the long gap between the end of Gemini and the start of Apollo/Saturn IB flights, or as a contingency to beat the Russians around the moon if Apollo suffered severe delays. But Von Braun and others were not interested in Congress getting wind of anything that could undermine support for Apollo. On June 8 NASA headquarters issued instructions that "any circumlunar mission studies related to the use of Gemini will be confined to in-house study efforts" and prohibiting issuance of contracts to McDonnell to pursue the matter.

Gemini/Transtage-LEOGemini/Transtage-LEO - Translunar Gemini with Double Transtage - LEO Configuration

Credit: © Mark Wade. 4,989 bytes. 635 x 251 pixels.

June 1965 - Gemini / Double Transtage

Still the matter would not die. A year later, astronaut Pete Conrad conspired with Martin and McDonnell corporations to advocate an early circumlunar flight using Gemini. Discretely called 'Gemini - Large Earth Orbit', the plan would use a Titan 3C-launched Transtage to boost the Gemini to translunar speed. A declassified memorandum from the Director, Gemini Systems Engineering, documents a June 24, 1965 meeting at Manned Spaceflight Center between the contractors' corporate heads and highest NASA management. At this meeting the companies provided a detailed proposal to launch a refurbished, modified Gemini around the moon by April 1967 for $ 350 million. The Gemini would have 521 kg of mass deleted, half of it by removing the solid fuel retrograde rockets used to initiate re-entry (the liquid fuel Orbital Manoeuvring System would be reengineered to increase its reliability). The Titan 2-launched Gemini would rendezvous and dock with a Titan 3C-launched 'Double Transtage'. The Double Transtage consisted of an unmodified first Transtage that would place itself and a second Transtage into low earth orbit. The first Transtage retained the navigation and manoeuvring systems necessary to move the assembly to the rendezvous orbit with Gemini. The second Transtage would be stripped of unnecessary equipment (the orbital manoeuvring system) but was equipped with an Agena-type docking collar.

After docking with the Double Transtage, the first Transtage would be cast off and the second Transtage would propel the Gemini into a circumlunar trajectory. The flights themselves, assuming go-ahead was given in September 1965, would follow immediately after the last Gemini flight. In December 1966 a Titan 3C would drive a 2450 kg circumlunar Gemini capsule to 11 m/s re-entry velocity to verify the heat shield design. This would be followed by a February 1967 manned qualification flight in earth orbit. A manned Gemini would dock with a Double Transtage and be propelled into a high orbit and re-entry speed. In April the sequence would be repeated, this time the Gemini being sent by Transtage into a loop around the moon.

Gemini/Transtage-TLIGemini/Transtage-TLI - Translunar Gemini with Transtage - Translunar Configuration

Credit: © Mark Wade. 3,548 bytes. 437 x 223 pixels.

The author of the memo thought that Gemini extension efforts would be better directed towards proving space station assembly techniques and procedures using Gemini and Agena. He also thought the schedule and cost estimates to be over-optimistic. The reaction of top NASA management was more categorical. Pete Conrad managed to stir Congressional interest, but NASA administrator James Webb informed them that any extra funds Congress cared to appropriate for such a project would be better spent accelerating the Apollo program. After further internal struggles, Conrad finally got NASA approval for the Agena on his Gemini 11 flight to boost him into a record 1,570 km orbit. This high flight was the only remnant of lunar Gemini.
April 1967 - Gemini Universal Lunar Rescue Vehicle

In the wake of the Apollo fire, NASA reexamined many safety aspects of the Apollo project. The Apollo mission profile was inherently risky, and the likelihood of a crew being stranded in lunar orbit or on the lunar surface was relatively high. McDonnell returned to a concept first studied in 1962 - the use of Gemini as a Lunar Rescue Vehicle. Use of the Gemini B capsule, then in construction for use with the US Air Force's Manned Orbiting Laboratory, with various combinations of Apollo lunar module stations, would provide a rescue vehicle that could pick up Apollo astronauts stranded in lunar orbit or on the lunar surface. Three variant rescue schemes were studied:

McDonnell summarised the advantages of the various schemes, as contrasted with use of Apollo hardware for the same task, in the following matrix:

Gemini Lunar SSSGemini Lunar SSS - Drawing of the Gemini Lunar Surface Survival Shelter. The shelter would be landed, unmanned, near the landing site of a stranded Apollo Lunar Module. In the event the LM ascent stage would not light to take the crew back to the Apollo CSM in lunar orbit, the two astronauts could go to the shelter and await a rescue mission. The astronaut in the CSM would return alone in the Apollo spacecraft.

Credit: McDonnell Douglas. 28,505 bytes. 522 x 395 pixels.

Lunar Orbit RescueLunar Surface Survival ShelterLunar Surface Rescue
Vehicle DescriptionModified Gemini & repackaged LM Ascent StageApollo CSMModified Gemini & Modified LM Descent StageModified SM & Modified LMModified Gemini, repackaged LM Ascent Stage & Modified LM Descent StagesApollo CSM & LM
MissionUnmanned to lunar orbit, three man direct returnUnmanned to lunar orbit, three man direct returnUnmanned to lunar surface, 28 day quiescent storage, 28 day 2-man operationUnmanned to lunar surface, 30 day manned operationUnmanned to lunar orbit, 30 day unmanned quiescent stay, 2 man direct returnUnmanned to lunar orbit, LM to lunar surface, LM to lunar orbit, 2 man return
Uses developed equipment

No new development
Can be accomplished with current acquisitions

Extension of lunar orbit vehicle

Similar to planned post-Apollo exploration shelter

Extension of lunar orbit/shelter vehicle
No rendezvous required
Direct return

No new development
Same as existing mission
New spacecraft development

Possibility of same failure mode

New spacecraft development

Requires modifications to existing hardware

New spacecraft development

Rendezvous required
May be difficult to automate transpose docking
RecommendationsDo not develop-rescue capability too limited. Greatest emergency potential at lunar surfaceDo not develop - need for shelter and total number of Saturn launches reduced by providing an on-station backup return capabilityModify to a 'Universal' Rescue Vehicle by improving capability to cover three-man cases

Gemini Lunar SRSGemini Lunar SRS - Gemini Lunar Surface Rescue Spacecraft. This spacecraft would be piloted by two crew to a landing near a stranded Apollo lunar module. The extended Gemini reentry capsule had a passenger compartment for the two rescued astronauts. The LSRS used three Lunar Module descent stages for lunar orbit insertion, lunar landing, and lunar ascent.

Credit: McDonnell Douglas. 51,464 bytes. 538 x 408 pixels.

McDonnell concluded that an unmanned Gemini 'Universal Lunar Rescue Vehicle' could be developed that would perform all three tasks. The Gemini capsule would be extended to allow up to three rescued Apollo crew members to be returned. Such a craft could rescue the entire Apollo crew at any point along the Apollo mission profile. Some sketches appear to show a two-man Gemini crew in addition to three crew couches in the Gemini capsule extension. The unspoken point was that the Saturn V was in fact large enough to land men on the moon using the direct-ascent method. Use of lunar orbit rendezvous was only necessary because of NASA's adherence to the 6 tonne, three-crew Apollo command module design. The 2 tonne Gemini capsule, even in a form stretched to accommodate three to five crew, could accomplish a direct landing on the moon using Apollo components.

This last attempt to resuscitate Lunar Gemini failed as well. At that point in the Apollo program cut-backs already had begun. No funds would be forthcoming to build additional launch vehicles and spacecraft beyond those already purchased. There was definitely no money to provide a rescue capability, using either Apollo or Gemini hardware.

A Personal Postscript

Not considered at the time, but truly having the potential for a reduced-cost, reduced-risk program would have been a purely Titan-based, USAF-managed project. By using earth-orbit rendezvous and Titan 2 and Titan 3C as the launch vehicles, a program can be constructed that would have landed an American on the moon much earlier than Apollo. With a 2,500 kg open-cockpit LM the moon landing could be accomplished using only two Titan 3 launches: one a Titan 3E, putting a Centaur upper stage into low earth orbit; the other a Titan 3D, putting a Lunar Gemini-LM combination into low earth orbit, which would dock with the Centaur and then proceed to the moon. Such a program, taking into account the actual Gemini and Titan 3C development schedules, would have looked something like this:

Gemini Lunar SRSGemini Lunar SRS - Alternate configuration for a Gemini Lunar Surface Rescue Vehicle. In place of 3 LM descent stages , this version uses 2 Apollo Service Modules and a repackaged LM descent stage. The first SM completes the translunar injection begun by the S-IVB stage. The second SM brakes into lunar orbit and then acts as a 'lunar crasher' stage, burning out just above the lunar surface. The third stage hovers to a landing near a stranded lunar module, and later boosts the Gemini capsule intotransearth trajectory.

Credit: McDonnell Douglas. 26,593 bytes. 546 x 315 pixels.

Apr 1964Gemini 1Titan 2Unmanned booster orbital test; boilerplate spacecraft.
Jan 1965Gemini 2Titan 2Unmanned suborbital test of spacecraft
Mar 1965Gemini 3 Titan 2Manned orbital 
Jun 1965Gemini 4Titan 24-day manned orbital
Jun 1965Gemini L-1Titan 3CFirst test flight of Titan 3C; unmanned lunar flyby
Aug 1965Gemini 5Titan 28-day manned orbital
Oct 1965Gemini L-2Titan 3CUnmanned lunar flyby test; Transtage exploded
Dec 1965Gemini 7Titan 214-day manned orbital
Dec 1965Gemini 6Titan 2Rendezvous with Gemini 7 (Agena target failed to orbit)
Dec 1965Gemini L-3Titan 3CUnmanned lunar flyby
Mar 1966Gemini 8 Titan 2/Atlas-AgenaAgena docking
Jun 1966Gemini 9 Titan 2/Atlas-AgenaAgena docking
Jun 1966Gemini L-4Titan 3CManned lunar flyby
Aug 1966 Gemini 10Titan 2/Atlas-AgenaLM docking
Aug 1966Gemini L-5Titan 3ETitan 3E test; unmanned; failure
Oct 1966 Gemini 11Titan 2/Atlas-AgenaLM docking
Nov 1966Gemini L-6Titan 3EUnmanned lunar orbiter
Jan 1967Gemini L-7Titan 3EManned lunar orbiter
Apr 1967Gemini L-8Titan 3E/Titan 3DManned earth orbit rendezvous, lunar orbit, LM descent
Jul 1967Gemini L-9Titan 3E/Titan 3DFirst landing on moon

Gemini ULRV MissionGemini ULRV Mission - Mission Summary for Gemini Universal Lunar Rescue Vehicle.

Credit: Mark Wade. 9,018 bytes. 715 x 559 pixels.

Such a program could have achieved a manned lunar landing two years earlier than Apollo at half the cost, a savings of $ 9 billion.

Gemini-Centaur-LMGemini-Centaur-LM - Gemini for lunar landing with Centaur and Langley open cockpit Lunar Module

Credit: © Mark Wade. 2,613 bytes. 632 x 143 pixels.

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Last update 12 March 2001.
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