Was a Manned Mars mission in 1982 feasible?

It's too risky is all you've got? Going to the Moon in 1969 was too risky. Landing was too risky. Taking off from the surface and docking in orbit was too risky. And so on.

If you want your SF art to become real then you actually do too risky. All of those X planes were too risky but they were flown - successfully. The SR-71 became operational.

You fly three spacecraft to Mars. One contains astronauts, and fuel can be made from the atmosphere. One contains supplies and can double as a return to orbit vehicle. A third contains spare parts and enough fuel to return to Earth. Before astronauts land, you get the ground supplies on the ground. It can be done.
 
It's too risky is all you've got? Going to the Moon in 1969 was too risky.
Apollo 15 and 17 were the longest Moon missions: 12 days exposure of the crew to cosmic radiation. A 1982 round trip mission to Mars would have taken 2-3 years, maybe even more. That is a different magnitude of risky, even if you only take crew health into consideration.

A certain Hyman G Rickover said this when discussing risk in the context of the US Navy's nuclear submarine development:
"Optimism and stupidity are nearly synonymous"
 
Apollo 15 and 17 were the longest Moon missions: 12 days exposure of the crew to cosmic radiation. A 1982 round trip mission to Mars would have taken 2-3 years, maybe even more. That is a different magnitude of risky, even if you only take crew health into consideration.

A certain Hyman G Rickover said this when discussing risk in the context of the US Navy's nuclear submarine development:
"Optimism and stupidity are nearly synonymous"

Interesting perspective. If you want space exploration then you find ways to minimize or eliminate the risk. Or just don't do it.
 
Apollo 15 and 17 were the longest Moon missions: 12 days exposure of the crew to cosmic radiation. A 1982 round trip mission to Mars would have taken 2-3 years, maybe even more. That is a different magnitude of risky, even if you only take crew health into consideration.

A certain Hyman G Rickover said this when discussing risk in the context of the US Navy's nuclear submarine development:
"Optimism and stupidity are nearly synonymous"
Honestly, the easiest solution to the background radiation issue is to select a crew that's never flown before - and never fly them again afterwards. They'll get close to the lifetime exposure limit for radiation workers, but probably won't exceed it. Dose rates are low enough that concerns about prompt radiation effects are negligible.

Something like a solar flare is a much bigger issue. Low probability, but it's a potential loss-of-crew scenario. You can provide protection, but at a certain point the risk can't be reduced further.

What's the risk appetite? Probably lower in 2024 than in 1970.
 
It was felt to be technically feasible by a bunch of engineers. But those engineers failed to recognise that Apollo's level of national support wasn't going to be sustained through to the end of the Apollo programme, much less for several more decades.
That part isn't really the engineers job. Someone asked them "how could we?", and they answered, " Probably something like this". The budget isn't in their hands, and if someone asked, "can we do it more cheaply if we took more risks", they'd probably come up with possible solutions increasingly more risky until saying, "it can't be done".

You're completely right that the cost would have been immense, and that support for that didn't exist. He already notes that in the opening post.

But if they threw enough money at it, they'd probably get something that could work. Not guaranteed to work, but reasonably capable of completing that mission. Even the Saturn V had limits, so it'd have to be broken down into manageable chunks of payload. As someone noted already, it'd mean prepositioning much of the material and supplies, plus a few extra for good measure, so when the crewed mission got there, they have everything needed for their decent and return trip already in orbit. It'd be many, many launches over many years, and many, many more dollars for each.

Technically feasible in 1982, yes. IF they had spent money during the 70's to develop the systems needed for that goal.

If you asked them to do it in 1982 with what was at hand, I very much doubt it, at least in a manner that had acceptable political risk for loss. A shoe string, hail-mary of such urgency that high risk for loss of life was viewed acceptable, maybe. Not sure how to MacGuffin that into 1982.
 
That part isn't really the engineers job.
The trouble they had was that too many tiers of management were filled with engineers who still thought worrying about that kind of thing wasn't their job. They hadn't realised they weren't really in engineering roles any more.

If you asked them to do it in 1982 with what was at hand, I very much doubt it, at least in a manner that had acceptable political risk for loss. A shoe string, hail-mary of such urgency that high risk for loss of life was viewed acceptable, maybe. Not sure how to MacGuffin that into 1982.
I think there's a huge difference between 1982 and 1986, which are the two dates most often quoted. 1982 is probably only possible under extreme duress; 1986 gives about 50% more time to work out the risks.
 
There was a simple solution to make it doable in 1982, Project Orion. Go fast enough and most problems become smaller.
 
Yeah, the zillion links make no sense in terms of what is technically feasible and what is not.
There are going to be technical problems, no doubt about it; there are a million risks; there is not necessarily a good reason to expend blood and treasure getting to Mars.
But there are a zillion ways to attack the various technical problems, and, as has been mentioned before, it is important not to confuse technical feasibility with political/economic/moral/risk-related feasibility.
 
Hi,
Similar to the Apollo Missions to the Moon, any planned trip to Mars could be viewed as large overall mission made up of many smaller individual tasks. For the Apollo missions this included issues like*;

  1. safely getting heavy loads into Earth orbit
  2. docking the command module to the lunar lander module
  3. exiting Earth orbit with the combined command module/lander assembly
  4. safely transitting from the Earth to the Moon
  5. entering luner orbit
  6. disengaging the lander from the command module
  7. safely descending in the lander to the Moons surface and executing a safe landing on the Moon
  8. doing whatever mission planned for the Astronauts that landed
  9. relaunching the upper stage of the lander into Lunar orbit
  10. redocking with the Command Module and transferring everyone back onboard
  11. exiting Lunar orbit
  12. safely transitting back from the Moon to the Earth
  13. re-entering Earth orbit
  14. jettisoning the lander and service modules
  15. safely deorbiting the Command module
  16. safely deploying the parachutes
  17. surviving rentry
  18. splashdown
Each of the steps above involved some degree of risks, and although the engineers and scientists could not necessarily identify all risks involved, there were likely mitigation strategies and contingency plans for if there were any number of issues during these steps. For instance, if something went wrong that either prevented docking with the Lunar Lander module or if there was an issue that prevented the combined Command, Service and Lander modules from safelty entring Lunar orbit, then there was always a possibility of aborting the restof the mission and returning to Earth, since the distances were not too far, as compared to the distance between the Earth and other planets, etc. Even so though, the accident on Apollo13 demonstrated that there could always be unforseen circumstances and evn the relatively short distance btween the Earth and the Moon could potentially be problematic if the life support systems were impacted.

Many years ago I had a video game called "Buzz Aldrin's Race Into Space" which was based on a board game called "Lift Off", and while these games simplified some issues and potentially chaned some stuff for playbilty purposes it was still a very good tool for demonstrating how a mission to the Moon could be viewed as a complex series of smaller steps. And in particular one of the big things the games stressed was that by conducting preliminary intermediary missions to test out some of these steps prior to doing a full mission to the Moon, experience could be gained and risks could likey be reduced or mitigated.

For the Apollo missions in particular, this included;
  • Apollo 4 - an unmanned launch of the Saturn V rocket
  • Apollo 5 - the first flight testof the Lunar module
  • Apollo 6 - a final uncrewed qualification test for the Saturn V
  • Apollo 7 - first crewed flight (with a 10 day duration)
  • Apollo 8 - first Apollo flight around the Moon
  • Apollo 9 - firstflight of the full Apollo spacecraft
  • Apollo 10 - test of all components for the lunar mission,with the exception of an actuallanding
  • Apollo 11 - first manned landing on the Moon
(source: https://www.nasa.gov/the-apollo-program/)

A mission to Mars could similarly be broken into smaller such steps as outlined above for the Lunar mission, and I would likely expect that while some experiences from the Apollo missions could be used to mitigate the risks of some of the steps, I would still expect that there would likely be the need for a number of "preliminary intrmediate missions" to test out systems and procedures.

For a mission to Mars there are also additional considerations that might need to be addressed such as "timing" since the distance between the Earth and Mars varies as each planet revolves around the Sun in their respective orbits. As such, if a proposed Mars mission involved sending multiple rockets launched at different times, then some consideration would likely need to be given to when each rocket is launched and whether it would be desirable to ensure that the rockets with the "supplies for while on Mars" or the rocket with the "Lander" safely make it to Mars orbit prior toactually lanching the astronauts (or not).

Also, since the distances to Mars could make a journey just to the planet a matter of many months (perhaps up to 9 or so), then "off ramps" in the event of a potential mishap have the potential for being radically different than for a Lunar mission. Specifically, for example if we are assuming a mutli-rocket approach with one rocket carrying the crew,one carrying supplies for when on the planet and one carrying the lander, and if a one way mission to Mars may take up to 9 months will the rocket carrying the astronauts need to potentially need to carry 18months worth of supplies to allow the crew to return to Earth in the event of any issues that may prevent that rocket from rendezvousing with the other rockets at Mars?

As such, ifwe really want to be serious bout trying to assess whether a manned mission to Marscould have been done in the 1980s, a reasonable starting point might be to
  1. decide on what type of mission is being considered (ie will there only be one rocket to carry everything, or would a singlemission consist ofmultiple rockets carrying varous components)
  2. estimate what kind of new hardware may need to be developed (ie will the planned mission require the development of larger/heavier lift rockets, will it require the assembly of anything in Earth orbit (such as using smaller rockets to lift compenents into Earth orbit to assemble a craft that would make the transit to Mars), and/or willit require newer more advance life support and recycling systems, or advanced concepts for sheilding the carft and crew from long twrm exposur to radiation.
  3. estimate potential time frames for developing and new equipment required
  4. estimate whether any "intermediate test flights" are required for this new equipment
  5. etc
My suspicion is that if we use the landing of Apollo 11 on the Moon as a starting point for planning a mission to Mars the 11 years from 1969 to 1980 is likely no where near enough time to do everthing likelt needed,and even if we instead assume a period of 20 years (1969 to 1989) it still likely isn't enough.

* I'm sure that there are a lot of other steps as well,but this is just meant to show some of the main ones that entailed potential risks
 
The US government went from producing zero atomic weapons to a thousand thermonuclear weapons a year in a decade, and went from Mercury-Redstone to Apollo 11 in a similar timeframe.

This is not going to be a "modern" effort conducted with an eye to cost control and risk management, or a private sector program with serious cost constraints, requirement for profitability at intermediate steps, and desire for great flexibility due to unclear market requirements, this may very well be conducted along the lines of a damn-the-torpedoes crash program.

With sufficient resources, parallel programs, and vast expenditures, impressive industrial efforts are quite possible in very short timeframes.

decide on what type of mission is being considered (ie will there only be one rocket to carry everything, or would a singlemission consist ofmultiple rockets carrying varous components)

We have a template; the Integrated Program Plan.



This was presented to Nixon by NASA in 1969, calling for a Mars landing by the 1980s. NASA officials considered it technically feasible and achievable within ten to twenty years. Nixon considered it politically and economically unwise (to say the least), and nixed it. The Mars program was not tied to any specific date, but it was believed that it could have been done by the early 1980s.

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On a side note, thousands of tonnes of water is ridiculous; you'd have a water recycling system set up. There were lots of ideas for that being worked on through the decades.
That's because you're using a lot of water for many different things.

4 liters per person per day for hygiene, minimum. 4 more liters per person per day for food and drinking. You can directly recycle about 6 liters of that (hygiene and food) per day, but need to condense the last 2 liters out of the air.

At least 50cm thickness of water for your storm cellar for radiation protection, and more like 1m thickness, and that's around a 3m diameter by 1 meter per crew count long shelter (trying to give the crew enough space to not immediately drive each other crazy if they're stuck in the storm shelter for more than a few hours). That adds up mass in a hell of a hurry, but is convenient to have for life support and all the other stuff as basically a freebie because you already have all that water for shielding.

Mission crew of at least 4, and 12 is better. Mission crew of 4 means 2 mechanics, 2 medics. That's just to get people there and home again. No trained pilots. Or at least not flying as their primary task. They'd have to be very cross-trained, I'm assuming that the mechanics would be taught how to do whatever manual flying would be required and that the medics would be taught how to do whatever other science stuff was wanted. Not that a mechanic can't get the samples, but the two career fields encourage different thinking patterns.

A crew of 8 and you can maybe have an actual geologist or two with you to know what samples would be interesting to take, in addition to 3 medics and 3 mechanics. A crew of 12 people lets you take a couple more scientists with you, but still half the crew is medics and mechanics to fix crew or ship in case of damage. And nobody goes outside without both a medic and a mechanic with them.

This means a really big ship, and a heavy one at that due to the water. You'd leave most of those tonnes of water in orbit, because you don't want to try to launch with all that weight to get home. You're still going to need 10-20kg of water per person assuming 100% recycling. And since you're going to be there or en route for years; ~8.5 months travel there via Hohmann Transfer orbit, ~16 months there for the next Hohmann window to open up, and 8.5 months back; you need a lot of water for losses as you go in and out of the airlocks etc.

So yes, you're going to have a crapton of water with you, between storm cellar and expected losses for 16 months on the surface.
 
That's because you're using a lot of water for many different things.
NASA life support systems studies from the 1970s and 80s ballpark life support mass per crew member in the five plus tonne range, and that includes consumables AIUI.

You need gobs of water, significantly more water than the body weight of the crew, but a thousand tonnes is waaay out there.


Your radiation shielding doesn't need to be all water either, the typical storm cellar is lined with all the mission supplies you need. Water is just one handy choice.

If you want even more water, look up Spacecoach and related proposals; that's honestly in the running for Mars and long term space development (looking at you Elon). Water propellant for the electric arcjet rockets, water for drinking, water for life support, water for radiation shielding, integration of propellant tank and radiation shield etc.

TLDR, the idea you describe is one possible approach to the system design, with interesting advantages, but not the one favored in 1969, when they were thinking classical storm shelters, water recycling systems, and LH2 propellant for NTRs.


Screenshot_20241127_140639_Adobe Acrobat.jpg

Representative example life support systems; a twelve man lunar base with a two year mission time needs on the order of a forty tonne life support system. This is on the order of a few tonnes, perhaps ten tonnes per head if we are to be pessimistic, not a hundred tonnes per head.

Screenshot_20241127_141243_Adobe Acrobat.jpg

Heck, even in the scenario where your system is open, with no recycling of water or air(!), your three year mission for four crew is only 150 tonnes of consumables, roughly forty tonnes of consumables per head! The benefits of recycling water are huge for long missions, and it's basically a given that that's how you will tackle the problem.
 
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Our spaceships are pathetic, still using the propulsion technology devised by Thiolkoswky and perfected by von Braun in the last century. We are still in the age of sailing, at the mercy of winds and currents, without propulsion for 99% of the trip. It's stupid to send humans on such a dangerous journey for no good reason... and there isn't.

Crossing the Atlantic on a sailboat is a dangerous sporting adventure, crossing it on the Spirit of St. Louis an absurd and dangerous record, crossing it on the Titanic an accident... But that was on the right track because its builders had good business reasons for what they were doing. What are the reasons for a manned trip to Mars?
 

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We are still in the age of sailing
The Polynesians crossed the Pacific, hop by hop, with big outrigger canoes, pigs, chickens, coconuts, and some understanding of the constellations.

How far did they go? From Taiwan, they settled the Pacific from Easter Island to New Zealand to Hawaii, and westward they got as far as Madagascar!

It's even in the Disney movie Moana!
(Of note are Moana's animal companions, a pig and a chicken).


This comparison is ancient, the same arguments have been trotted out in circles and nauseum, we've been talking about this again and again for the past fifty darn years. Jerry O'Neill wrote the High Frontier in what was it, 1975?

l5-news-resources-of-space (2).gif

This comic is from '81; it is 43 years old! Note the outrigger canoe. The man in the watchtower is suggesting that the canoe be used to attack the other side of the island.
 
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What are the reasons for a manned trip to Mars?
Tunguska. Chicxulub. Shoemake-Levy 9. The iridium in the K-T boundary.

Asteroidal impacts that would result in the end of human life on earth.

The point is to get humans off Earth so that one asteroid does not end all human history.

Humans on Mars is simply the first step.
 
The Polynesians crossed the Pacific, hop by hop, with big outrigger canoes, pigs, chickens, coconuts, and some understanding of the constellations.

How far did they go? From Taiwan, they settled the Pacific from Easter Island to New Zealand to Hawaii, and westward they got as far as Madagascar!

It's even in the Disney movie Moana!
(They even snuck in the pig and the chicken).

All great human migrations have had a good reason: fleeing wars, oppressive governments or overpopulation and hunger, no one embarks with their family, their animals and their scarce properties on a stupid romantic adventure of exploration.
 
Tunguska. Chicxulub. Shoemake-Levy 9. The iridium in the K-T boundary.

Asteroidal impacts that would result in the end of human life on earth.

The point is to get humans off Earth so that one asteroid does not end all human history.

Humans on Mars is simply the first step.
I do not agree, the first step should be to establish numerous orbital colonies equipped with artificial gravity by rotation, independent of the Earth and with their own propulsion systems to avoid the worst of solar flares by taking refuge behind a planet or moon.

That will only be possible when quantum technology is developed that allows photosynthesis to be duplicated to create food from sunlight and obtain water and other elements from asteroids and comets. Then we will be safe from everything except a nearby nova.

Mars is even less safe than Earth, having no atmosphere or magnetic field to protect against radiation.

Mars is not the promised land, it is a death trap... ask the Vikings of Greenland.

 
I do not agree, the first step should be to establish numerous orbital colonies equipped with artificial gravity by rotation, independent of the Earth and with their own propulsion systems to avoid the worst of solar flares by taking refuge behind a planet or moon.
Yes, I expect that will be the first part of building the Mars colony ships.


That will only be possible when quantum technology is developed that allows photosynthesis to be duplicated to create food from sunlight and obtain water and other elements from asteroids and comets. Then we will be safe from everything except a nearby nova.
Why duplicate photosynthesis when you can literally just grow plants? Careful selection of plants to not require flying insects for pollination makes life pretty easy. Add some fish to the hydroponics, like the rice paddies and their fishy co-inhabitants. Maybe chickens, if you can handle the bird poop issues (which just goes back into the hydroponics once it's aged).


Mars is even less safe than Earth, having no atmosphere or magnetic field to protect against radiation.

Mars is not the promised land, it is a death trap... ask the Vikings of Greenland.
Mars is where you go to develop the technologies for reliable long term habitation systems. Luna isn't terrible, but is a little too exposed and has a very high surface radiation issue.
 
The idea of using water as an anti-radiation shield dates back to 1939, we need some kind of very effective electromagnetic generator that is capable of stopping the worst ultra-high energy particles that will surely one day reach one of our ships destroying its electronics.

We need the Vulcans to come and tell us that we are not yet ready or we are going to be responsible for our own means?
 

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no one embarks with their family, their animals and their scarce properties on a stupid romantic adventure of exploration.

"See the line where the sky meets the sea, it calls me!!!"

View: https://youtu.be/cPAbx5kgCJo?feature=shared


There have always been humans imbued with a degree of adventurousness and wanderlust, forging ahead for stupid romantic reasons. The Americans traditionally value this spirit of adventure and educate their children accordingly, which was why it was made a central theme of the Disney princess movie Moana.

While often irrelevant, adventurers have long established paths that may subsequently be followed by larger parties and organizations. Some degree of human space exploration and settlement is highly probable.

The current trajectory is supportive, you already have some cults and eccentrics planning to settle Mars.

Now whether or when this will happen or whether it will translate into a broader human use of space is another matter entirely.

And no, Mars is a horrible testbed. The Moon is far better; much closer and with much more frequent launch windows. You can iterate on stuff in the span of weeks, not years - if the ISRU liquid oxygen maker is not working, you can redesign/debuf it and ship a new one up in as little as two weeks, upon which you can see whether the new one works, whereas you'd have to wait two and a half years for the planets to align if the machine was found to be buggy on Mars - and that's before the what, six month flight time?

The iteration cycle for the Moon is much, much shorter, which is why the Chinese were able to do Chang'E missions every year or two, improving the design every time. Very difficult with Mars or asteroid missions.
 
Mars is not the promised land, it is a death trap... ask the Vikings of Greenland.
I agree.

As Scott noted, there are strategic reasons to invest in space flight tecnology, but orbital stations could work as life preservation arks in case of an incoming massive extinction event.

I see human landing in Mars as a "romantic" mission, there are no value on it.
Instead, I think there are most profitable steps to follow in the Solar System exploration.
Solar System population is a concept that makes little sense to me. I agree again with Justo.
 
"See the line where the sky meets the sea, it calls me!!!"

View: https://youtu.be/cPAbx5kgCJo?feature=shared


There have always been humans imbued with a degree of adventurousness and wanderlust, forging ahead for stupid romantic reasons. The Americans traditionally value this spirit of adventure and educate their children accordingly, which was why it was made a central theme of the Disney princess movie Moana.

While often irrelevant, adventurers have long established paths that may subsequently be followed by larger parties and organizations. Some degree of human space exploration and settlement is highly probable.

The current trajectory is supportive, you already have some cults and eccentrics planning to settle Mars.

Now whether or when this will happen or whether it will translate into a broader human use of space is another matter entirely.

And no, Mars is a horrible testbed. The Moon is far better; much closer and with much more frequent launch windows. You can iterate on stuff in the span of weeks, not years - if the ISRU liquid oxygen maker is not working, you can redesign/debuf it and ship a new one up in as little as two weeks, upon which you can see whether the new one works, whereas you'd have to wait two and a half years for the planets to align if the machine was found to be buggy on Mars - and that's before the what, six month flight time?

The iteration cycle for the Moon is much, much shorter, which is why the Chinese were able to do Chang'E missions every year or two, improving the design every time. Very difficult with Mars or asteroid missions.
The second generation of Lunar and Martian colonists will not be able to live in Earth's gravity, they will be mutants and no one knows what unknown diseases they will develop, whoever goes will not be able to return.
 
I agree.

As Scott noted, there are strategic reasons to invest in space flight tecnology, but orbital stations could work as life preservation arks in case of an incoming massive extinction event.

I see human landing in Mars as a "romantic" mission, there are no value on it.
Instead, I think there are most profitable steps to follow in the Solar System exploration.
Solar System population is a concept that makes little sense to me. I agree again with Justo.
es un honor:)
 

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At first humans believed that the sun, moon and lightning were gods and the Earth was flat, then they believed that all the stars revolved around the Earth attached to a glass sphere, then they believed that there were no planets around other stars, then they discovered that galaxies existed and many dangerous and horrible things out there. How much do we still ignore?

We need an opportunity to learn how to fight space... Living in ... Know your enemy.
 

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Here we go again. "Is der any money in it? No? Den don't go." Simple, convenient.

Followed by looking wistfully at all your SF art.
 
Back in the early 1990s I was extraordinarily fortunate to attend a small lecture by Bob Zubrin, where he presented his "Mars Direct" plan to a room of mostly aero engineers from McDonnell Douglas. It required no new technology whatsoever, took into account the shielding requirements, and was a meticulous plan if ever I saw one. It was brilliantly elegant.

What happened? Well, NASA happened. Apparently the plan was too simple; it didn't meet their internal political needs. It totally bypassed their manned space station and lunar exploration organizations, and needed only minimal inputs from their advanced systems technologies experts. So over time, the whole beautiful elegant original concept, simple and inexpensive as it was, gradually grew into something that actually WOULD use NASA's cherished silo organizations. It became large, complex, expensive. And so of course, there was no budget to do anything so elaborate. And here we are today.

The Wikipedia article on Mars Direct actually does a good job of covering the original vision, and it's well worth reading.
 
I had forgotten about that. Here's the plan.


Scroll down to see a PDF of the original 1991 report.
 
There is an absolutely enormous amount of money in space based resource extraction.

"Yeah, we found an asteroid, pretty good gold yield, on the order of 500 grams per ton. The asteroid is over a million tons, we're talking about half a million kg of gold. In this one asteroid."

Insert any and all other materials as well.
 
Supply and demand. A lot of new gold means the price goes down. Perhaps it would be best to declare it "space use only." It would be earmarked for space-based, lunar and possibly Mars manufacturing use. It wouldn't be sent to Earth to lower mineral prices.
 
...
We have a template; the Integrated Program Plan.



...
Hi,
Realistically that template only represents one possible approach, and from what others have posted it appears that there may have been other approaches that would likelyalsoneed tobe considered.

In addition, from browing through the link provided it appears that this IPP plan was predicated on several assumptions that I'm not sure would have been really fully feasible at the time. Specifically, that plan appears to rely on designing, developing, and making operational "a reusable Nuclear Shuttle for LEO-GEO and LEO-lunar orbit transportation" by 1976 (if I am understanding correctly). Not only does this seem to be a very short time period to develope, build and make operational such a craft but one is left to wonder whether the thought of trying to use a "nuclear" craft in LEO might not face some serious hurdles.

Regards
 
Hi,
Realistically that template only represents one possible approach, and from what others have posted it appears that there may have been other approaches that would likelyalsoneed tobe considered.

In addition, from browing through the link provided it appears that this IPP plan was predicated on several assumptions that I'm not sure would have been really fully feasible at the time. Specifically, that plan appears to rely on designing, developing, and making operational "a reusable Nuclear Shuttle for LEO-GEO and LEO-lunar orbit transportation" by 1976 (if I am understanding correctly). Not only does this seem to be a very short time period to develope, build and make operational such a craft but one is left to wonder whether the thought of trying to use a "nuclear" craft in LEO might not face some serious hurdles.

Regards
Look up NERVA.

The rocket was ready for test flights. By the mid 1960s.

Launch the rocket into orbit before it first goes critical and it's relatively safe.
 

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