No. The same arguments apply; the increased cost, needed technology development to support a crewed landing mission, the amount of effort that is necessarily devoted to crew maintenance and health, et cetera. In fact, while the hypothetical scheduling of human missions is dependant upon minimizing Earth-Mars transit times, an uncrewed vehicle could use any interval for the interplanetary transit with minimial concern for exposure to the charged particle and energetic cosmic ray environments. This would allow more and sooner opportunies to launch missions and collect information that may facilitate later missions, both remotely operated and eventual crewed.
While just looking at the cost of a space mission versus combating poverty or illness is a false dichotomy (there are many other things we could reduce or eliminate to provide funding for social causes if we were so inclined) this does highlight the consideration that money spent on space exploration and development should provide a benefit to the population overall rather than just one narrow segment of scientists, aerospace interests, and enthusiasts. Access to precious space resources, Earth and solar weather surveillance, navigation and telecommunications, hazard abatement, et cetera are all things that have and will continue to benefit the population writ large (whether people realize it or not). Going to Mars is of very modest benefit for only a tiny portion of scientists. If the cost were small (as with current uncrewed missions) the expense can be justified as expanding our scope of knowledge; when the cost is so massive that it would detract from both other exploration programs and science funding in general, the onus is on supporters to demonstrate some tangible benefit in accordance with the cost.
Actually, in 2001: A Space Odyssey, there were definite national interests that actually drove the plot (and served to highlight the narrow thinking of humanity); the US discovered SMA-1 on the Moon and concocted an “embarassing” cover story about an infection to keep the Russians from learning about the monolith. The Discovery mission to Jupiter was modified with the scientists being placed in hibernation and the HAL 9000 ship’s computer being given a “secret directive” which caused it to go insane over the conflict of not informing the crew.
Realistically, an internationally crewed mission adds significant complexity in planning, funding, political decision-making, and priority, a situation demonstrated by international projects such as the ISS (although since the US has borne most of the cost it has made most of the decisions essentially unilaterally, often to the grumblings of other member nations), the Large Hadron Collider at CERN, and the International Thermonuclear Experimental Reactor (ITER) where it has been cited as a major cause of delays and cost increases. Since the cost of a crewed mission would also probably be largely borne by the US–no other nation has the assets or technical prowess to engage in such a mission alone–the bulk of a crew of six or twelve (depending on scale) would likely be half or more American, leaving limited slots for astronauts from other partner nations.
You continue to focus on the distance travelled by the Mars rovers as some kind of figure of merit even though I have repeatedly explained that the limited rate at which they travel is due to the limited power available and not any kind inherent restriction in robots. Yes, it is true that circa 1970 the best sample collection and return system we could devise was an astronaut but believe it or not the discipline of robotics and autonomous systems has advanced significantly since that time, and we routinely use robots in all kinds of applications such as mining, radio- and toxic material handling, explosive ordnance disposal, et cetera where the hazard and cost of using people is simply not justified. For the cost of even a simple high-risk short surface duration crewed Mars mission (~US$200B for a 30 day surface duration, or over US$100M per person-day of effort) we could literally pepper the surface of Mars from pole to equator to pole with robotic probes of various and multiple capabilities with far more vast range and much longer mission duration than any crewed mission could attempt.
For illustration, here is a comparison I made between the capabilities and limitations of a human astronaut versus the Mars Science Laboratory:
*Let’s make an apples to apples comparison between human astronauts and a robotic mobile science platform (rover) like the Mars Explorer Rovers:
Human Astronaut
On-Board Sensors: Mark I binocular imagers (effective feature resolution ~0.1mm), restricted bi-aural receptors, external signals transmitter/receiver
Manipulators: (2) five digit appendages enclosed in KevlarTM gauntlets with minimal tactile feedback
Communications: Auditory, hand-held or helmet-mounted camera
Control: Auditory commands only via multi-variant “ENGLISH” language; single on-board control system subject to malfunction by hypoxia, dehydration, malnutrition, or, contamination; complex autonomous internal codes (fear, anxiety, anger, depression) may interfere with optimum functioning
Power: Self-powered, requires complex balance of nutrients and potable water at several hour intervals
Operating Duration: 8-12 hours/day (effective maximum, depending on workload, fatigue)
Consumables: ~2 kg/day of carbohydrates, proteins, lipids, sterols, vitamins; 2 liters/day of liquid water; oxygen
Maintenance: Multiple daily waste removal; continuous removal of respiratory waste (CO2 < 1%); periodic external cleansing with mild solvent; routine examination for injury and buildup of self-producing toxins; external stress-relieving stimuli (entertainment)
Environmental Tolerance: 0-55 deg C (absolute limits), 14-30 deg C (optimum function); ppO2 0.2-0.8 bar; highly susceptible to chemical contaminants, ambient radiation, mechanical and acoustic shock
Reliability Requirements: Environmental and power sustainment required to be reliable >4 stdev throughout entire mission duration without interruption; support and delivery systems must be qualified to “man-rated” standards
Launch/Delivery Vehicle: One or more unspecified heavy lift launch vehicle; unspecified interplanetary transit vehicle with environmental sustainment and Earth-return capability for multiple (3+) exploratory units; unspecified surface landing and return module
Mars Science Laboratory (“Curiosity”)
On-Board Sensors: mast-mounted high definition multi-spectra cameras (MASTCAM), manipulator-mounted ultra high definition (0.014mm resolution) camera (MAHLI), X-ray diffraction system, pulsed neutron emitter (DAN), tunable laser spectrometer, alpha particle X-ray spectrometer, laser-induced breakdown spectroscope (ChemCam), gas chromatograph, quadrupole mass spectrometer, multiple sensors for navigation and self-diagnostics
Manipulators: High precision robotic manipulator arm with survey and sampling apparatus built-in
Communications: Redundant low- and high-bandwidth transmitters for command upload, precision diagnostic feedback, data return
Control: Precision command control via explicit (single value) instructions; semi-autonomous on-board redundant radiation-hardened computer (Rover Electronics Module) utilizing established operational and contingency protocols; ability to upload novel skill set via firmware patch
Power: Multi-Mission Radioisotope Thermoelectric Generator (MMRTG), 2.5 kWh/day
Operating Duration: Continuous operation for intended 2 year mission, MMRTG rated for 14 years output
Consumables: None.
Maintenance: Firmware uploads; no physical maintenance required
Environmental Tolerance: Design tolerance for anticipated mission environment conditions (-127 to 30 deg C, near vacuum atmosphere, ambient radiation) with standard qualification margins (+/- 10 deg C)
Reliability Requirements: >3 stdev (99.7% reliability) acceptable for mission duration
Launch/Delivery Vehicle: Atlas V (541) with Dual Engine Centaur upper stage/Earth Orbit Escape vehicle, aeroshell landing vehicle similar to Viking lander; no return vehicle required
There is no question that both the overall mission cost and the value of science per dollar spent is vastly greater with robotic probes, notwithstanding the emotional reluctance and ethics of placing human astronauts in harm’s way without taking extraordinary measures to reduce hazards. A rule of thumb about manned missions is that at least 90% of the effort is just keeping the “meat puppets” alive and functional, and a look at the historical costs of manned versus unmanned missions (not including launch costs) shows at least another order of magnitude difference in cost. That means that at best, for every dollar’s worth of science data you get from a robotic mission you’re getting one penny from a manned effort.*
This is notwithstanding the capabilities we could build into a larger Mars rover with a more capable power source and current technology, or the economies of scale of performing multiple parallel missions versus a single crewed mission to one or at most two landing sites, and the risk of complete loss of multi-hundred-billion dollar mission should the habitat or charged particle radiation protection systems fail for even a relatively short duration, and the near certainty in the case of failure that another very costly attempt would not be made in the foreseeable future.
The only real argument for performing a crewed mission in the near future against significant hazards that we can only poorly mitigate is that it would be “cool” or demonstrate national prestige. I like cool and think the US is pretty keen (although to be fair, I like New Zealand, Switzerland, and Okinawa a lot, too) but not to the tune of a cost that makes even a jaded politician cringe to say out loud, and not at the expense of doing other comparable exploration and science at a small fraction of the cost. The question isn’t really one of whether people are better in some abstract, “people can pick up things and touch stuff” sense; it’s essentially a problem of optimization, i.e. how can you do the most useful science and advance the general technology of space resource utilization for a given (realistic) budget. The answer is definitively not to spend a vast amount of money to do send people at high risk as soon as feasible in order to accomplish the same things that could be done as well or better and without incurring the cost of maintaining a narrow range of habitable conditions both on the journey there and return. That is just about the least optimial solution of all, and one that is far more likely to retard the ultimate development of human space habitation and exploration than to foster it.
Stranger