MediaWiki API result

This is the HTML representation of the JSON format. HTML is good for debugging, but is unsuitable for application use.

Specify the format parameter to change the output format. To see the non-HTML representation of the JSON format, set format=json.

See the complete documentation, or the API help for more information.

{
    "batchcomplete": "",
    "continue": {
        "gapcontinue": "Recreation",
        "continue": "gapcontinue||"
    },
    "warnings": {
        "main": {
            "*": "Subscribe to the mediawiki-api-announce mailing list at <https://lists.wikimedia.org/mailman/listinfo/mediawiki-api-announce> for notice of API deprecations and breaking changes."
        },
        "revisions": {
            "*": "Because \"rvslots\" was not specified, a legacy format has been used for the output. This format is deprecated, and in the future the new format will always be used."
        }
    },
    "query": {
        "pages": {
            "1170": {
                "pageid": 1170,
                "ns": 0,
                "title": "Ready For Mars Project",
                "revisions": [
                    {
                        "contentformat": "text/x-wiki",
                        "contentmodel": "wikitext",
                        "*": "''Ready For Mars'' is a project to develop a realistic and achievable [[Mission concepts|manned mission to Mars]]. <ref>[http://www.marsdrive.com/Libraries/MarsDrive_Documents/The_Mission4_1.sflb.ashx MarsDrive: Ready For Mars - Mars Mission Concept]</ref>\n\nHowever, by the end of 2019 the project Worksite no longer seems to be active, or has been merged with the Mars Initiative fund raising project and is no longer explicitly described.\n\n==Background==\n\n===Objective===\n\nThe Ready For Mars project aims to develop a practical engineering design for a manned mission to Mars, comprehensively addressing the various technological challanges that need to be overcome. This effort is based around an outline mission concept that aims to minimise the technological challenges involved.\n\n===Guiding Principles===\n\nThe stated guiding principles of the project are:\n\n''To conduct exploration of Mars with a view to establishing a permanent base and, ultimately and in the longer term, a settlement, using the simplest and most pragmatic mission design with the lowest development cost and timescales.''\n\n===History===\n\nThe ''Ready For Mars'' project originated from early work carried out by the MarsDrive consortium, with an online collaboration under the name MarsDrive Mission in April 2007. This mission aimed to build on Grant Bonin's ''Mars For Less'' proposal and had the objective of developing a mission using very small landers, to complement the small launch vehicles proposed by Bonin. During the development it became clear that the use of very small landers circumvented many of the Mars Entry, Descent and Landing difficulties that were a major stumbling block for more \"conventional\" missions employing landers massing many tens of tons.\n\nThe original MarsDrive work was further developed by Terry Wilson, later with the assistance of David Gooding, into an outline mission concept that represented a serious attempt to develop a practical mission design that could be achieved within the scope of conventional entry, descent and landing technologies.\n\nThe mission concept is currently in a draft form and work continues to complete the concept definition. The Ready For Mars project is aimed at completing the concept, conducting the necessary research and development into the technologies required and embarking upon a formal top-down engineering design for the various mission systems.\n\n==Mission Concept==\n\n===Overall Mission Characteristics===\n\nThe mission concept is characterised by:\n\n*Conventional, Viking-style, Entry, Descent and Landing technology\n*Small landed payloads (ca. 4,500 kg)\n*High redundancy of surface units \u2013 mission is a \u201cgo\u201d with any single landing failure (and most double failures)\n*High surface mobility\n*High science return (several thousand kg of scientific equipment)\n*Assured Return (that is, not a one-way mission)\n*Use of In-Situ Resource Utilization (ISRU) for ascent propellants, breathing air and water.\n*Objectives-focused design\n\n===References===\n<references />\n\n{{wikify}}\n\n [[category:Human Mission Architecture]]"
                    }
                ]
            },
            "7026": {
                "pageid": 7026,
                "ns": 0,
                "title": "Recent Liquid Flow on Mars",
                "revisions": [
                    {
                        "contentformat": "text/x-wiki",
                        "contentmodel": "wikitext",
                        "*": "==Recent liquid flow on Mars?== \nPhotographs of Hebes Chasma were recently published<ref>[http://spacefellowship.com/news/art35520/martian-scars.html \"Martian scars\" at SPACE FELLOWSHIP]</ref> which show considerable resemblance to [[Liquid Water on Mars|liquid flow]] features.  The dark stains seem to show something that \"pool[ed] like spilt ink\".  Commentator(s) bent over backwards trying to not seem to be guilty of sensationalism.  The stains were suggested to be probably dust movement that produced a \"flow-like feature\".  There is a possibility that wind can become heavily laden with dust and flow downwards to leave the dust collected in a broad flat pool, but the images in this case make that explanation seem unlikely.  The possibility of a petroleum seep suggests itself but the flow pattern that would result in the actual images is hard to imagine.  Perhaps some unknown dense gas of volcanic origin collected in Hebes Chasma and then condensed as dew on the surfaces that cooled the most by radiation.  This dew then slowly drained from those surfaces into inky pools in deep depressions in the eastern and central parts of Hebes Chasma.  If there is a liquid on Mars of petroleum nature, it could be an advantage for colonization efforts some day.  \n \n==Reference== \n<references /> \n \n[[Category:Areology]]"
                    }
                ]
            }
        }
    }
}