[QUOTE=Declan]
The ISS was Sapos suggestion after commenting on my reason for getting there. Since there is no off the shelf vehicle available, any fast mission to mars is going to involve a hybrid composite thats going to be made up most likely of parts that have been gathering dust in museums for the last 3 decades.
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Sorry, I didn’t mean to misattribute you.
Those “parts that have been gathering dust in museums for the last 3 decades” are not going to cut it for use, even improvisationaly. Even cutting out the bureaucracy, issues with aging and pedigree would make most stuff (say, Apollo-era hardware) unusable, and all of the support and maintenance equipment, plus many of the detail plans, are probably lost or destroyed. As someone who makes a living out of helping to refurbish and use decades-old, decommissioned rocket motors, I can assure you that trying to use equipment that has long disappeared from operational status with no aging and surveillence program is going to be more expensive and less trustworthy than just fabricating new.
A signficant amount of the technical difficulty of building a manned spacecraft are the thermal protection systems used for re-entry, hence the adoption of a blunt cone arse-first heat shield for the CEV/Orion replacement for the shuttle; it’s tried and proven, relatively cheap and easy to build and refurbish, and doesn’t require delicate, bleeding each material technology. Another are launch abort safety systems which are intended to give the crew a way to evac during and immediately after launch. In all honesty, these systems offer at best a marginal chance of successful escape during the early stages of boost. Eliminating these two systems and adopting a more risk-accepting stance regarding safety (i.e. we can’t prevent every possible problem, so we’ll focus on those that fall within a three sigma level of possibility) would dramatically reduce the cost and often unnecessary complexity of a vessel. Now you’re left with a habitat, shielding, power, provisions & recycling, shielding, and GN&C (guidence, navigation, and control). With the exception of propulsion and provisions & recycling, those are all soluable (given a sufficiently large bank account) with existing technology, and if you’re willing to accept the risk and hardship of a slow, lugubrious low-energy Hohmann transfer, you could get to Mars with only very modest extenions of existing technology.
I seriously doubt, however, that anyone can come up with a justification for needing to do so on short order that doesn’t amount to science ficiton, i.e. aliens, monoliths, et cetera. Even an incoming planet-killing meteor would be best dealt with one or more unmanned probes carrying large nuclear weapons or nuclear pulse rockets that would push the object out of the intercept course.
Stranger