Ready For Mars Project - Revision history

Michel Lamontagne at 20:58, 10 November 2020

2020-11-10T20:58:58Z

Michel Lamontagne: /* History */

2019-12-28T01:27:52Z

History

Michel Lamontagne: /* History */

2019-12-28T01:24:58Z

History

Jburk at 00:29, 18 December 2018

2018-12-18T00:29:32Z

Rfc: reference to the original project document added

2013-10-03T20:29:24Z

reference to the original project document added

Rfc: Undo revision 8504 by 201.252.84.145 (Talk)

2013-03-11T21:06:35Z

Undo revision 8504 by 201.252.84.145 (Talk)

201.252.84.145: /* Systems and Equipment */

2013-03-11T18:00:58Z

Systems and Equipment

Spriditis: multiple vandalisms

2011-11-05T14:27:32Z

multiple vandalisms

41.190.16.17: /* Mission Concept */

2011-11-05T04:43:51Z

Mission Concept

59.124.27.108: /* Overall Mission Characteristics */

2011-11-05T04:30:25Z

Overall Mission Characteristics

← Older revision		Revision as of 20:58, 10 November 2020
Line 1:		Line 1:
−	''Ready For Mars'' is a project to develop a realistic and achievable 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>	+	''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>

	However, 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.		However, 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.

@@ Line 1: / Line 1: @@
 ''Ready For Mars'' is a project to develop a realistic and achievable 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>
 ==Background==
@@ Line 20: / Line 22: @@
 The 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.
 ==Mission Concept==
@@ Line 38: / Line 38: @@
 *Objectives-focused design
-===Mission Overview===
+===References===
 <references />

@@ Line 20: / Line 20: @@
 The 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.
 ==Mission Concept==
@@ Line 33: / Line 35: @@
 *High science return (several thousand kg of scientific equipment)
 *Assured Return (that is, not a one-way mission)
 *Use of In-Situ Resource Utilization (ISRU) for ascent propellants, breathing air and water.
 *Objectives-focused design
@@ Line 43: / Line 45: @@
 ==References==
-<references/>
+<references />
 {{wikify}}
   [[category:Human Mission Architecture]]

← Older revision		Revision as of 00:29, 18 December 2018
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	{{wikify}}		{{wikify}}

−	[[category:~~Ready For Mars Project~~]]	+	[[category:Human Mission Architecture]]

@@ Line 1: / Line 1: @@
-''Ready For Mars'' is a project to develop a realistic and achievable manned mission to Mars.
+''Ready For Mars'' is a project to develop a realistic and achievable 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>
 ==Background==
@@ Line 41: / Line 41: @@
 ===Systems and Equipment===
 {{wikify}}
   [[category:Ready For Mars Project]]

← Older revision		Revision as of 21:06, 11 March 2013
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	===Entry, Descent and Landing Technology===		===Entry, Descent and Landing Technology===

−	Mias kai ta les ola afta pes kai gia th Benroubi thn evraia pou exei pfnarettei to Dhmou, to megisto ka8iki, ton arxiroufiano pou xarizei pote th makedonia, pote to aigaio. Oi kyrioi evraioi exoun onomata, ast tous xemprostiasoume kapote. Psoniste ta hlektrika sas stou Benroubi. Dwro mia menorah kai to teleftaio vivlio tou Dhmhtra!	+	===Systems and Equipment===
		+	{{wikify}}
		+
		+	[[category:Ready For Mars Project]]

← Older revision		Revision as of 18:00, 11 March 2013
Line 40:		Line 40:
	===Entry, Descent and Landing Technology===		===Entry, Descent and Landing Technology===

−	~~===Systems and Equipment===~~	+	Mias kai ta les ola afta pes kai gia th Benroubi thn evraia pou exei pfnarettei to Dhmou, to megisto ka8iki, ton arxiroufiano pou xarizei pote th makedonia, pote to aigaio. Oi kyrioi evraioi exoun onomata, ast tous xemprostiasoume kapote. Psoniste ta hlektrika sas stou Benroubi. Dwro mia menorah kai to teleftaio vivlio tou Dhmhtra!
−	~~{{wikify}}~~
−
−	~~[[category:Ready For Mars Project]]~~

← Older revision		Revision as of 14:27, 5 November 2011
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	The 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.		The 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.

−	~~At last! Someone who understands! Thanks~~ for ~~potsnig!~~	+	==Mission Concept==
		+
		+	===Overall Mission Characteristics===
		+
		+	The mission concept is characterised by:
		+
		+	*Conventional, Viking-style, Entry, Descent and Landing technology
		+	*Small landed payloads (ca. 4,500 kg)
		+	*High redundancy of surface units – mission is a “go” with any single landing failure (and most double failures)
		+	*High surface mobility
		+	*High science return (several thousand kg of scientific equipment)
		+	*Assured Return (that is, not a one-way mission)
		+	*Use of In-Situ Resource Utilization (ISRU) for ascent propellants, breathing air and water.
		+	*Objectives-focused design
		+
		+	===Mission Overview===
		+
		+	===Entry, Descent and Landing Technology===
		+
		+	===Systems and Equipment===
		+	{{wikify}}
		+
		+	[[category:Ready For Mars Project]]

← Older revision		Revision as of 04:43, 5 November 2011
Line 21:		Line 21:
	The 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.		The 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.

−	~~==Mission Concept==~~	+	At last! Someone who understands! Thanks for potsnig!
−
−	~~This ifnormatoin is off the hizool~~!
−
−	~~===Mission Overview===~~
−
−	~~===Entry, Descent and Landing Technology===~~
−
−	~~===Systems and Equipment===~~
−	~~{{wikify}}~~
−
−	~~[[category:Ready For Mars Project]]~~

@@ Line 23: / Line 23: @@
 ==Mission Concept==
-===Overall Mission Characteristics===
+This ifnormatoin is off the hizool!
 ===Mission Overview===