Thermal Effects - Drive - Revision history

MazonDel: Changed the content 'insert image...' to actually displaying the image.

2015-05-14T20:49:21Z

Changed the content 'insert image...' to actually displaying the image.

← Older revision		Revision as of 13:49, 14 May 2015
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	One common theorized source of the anomalous thrust is that thermal effects endemic to the structure or components of the activated drive may alter the center of mass or otherwise influence the thrust reading.		One common theorized source of the anomalous thrust is that thermal effects endemic to the structure or components of the activated drive may alter the center of mass or otherwise influence the thrust reading.

	~~Insert~~ image from ~~Reply #7 (~~RotoSequence) concerning the thermister data from the PZT Mach Effect Thruster ~~from page 1~~.		<img src="http://forum.nasaspaceflight.com/index.php?action=dlattach;topic=36313.0;attach=626461;image" style="width:30%">

			Above image from RotoSequence's post concerning the thermister data from the PZT Mach Effect Thruster. <ref>[http://forum.nasaspaceflight.com/index.php?topic=36313.msg1302018#msg1302018 RotoSequence's post.]</ref>

	== Status ==		== Status ==

Saucyjack at 22:03, 6 May 2015

2015-05-06T22:03:49Z

← Older revision		Revision as of 15:03, 6 May 2015
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	== Evidence Against ==		== Evidence Against ==
	#The thrust response is instantaneous while the thermal response is not.<ref>[http://forum.nasaspaceflight.com/index.php?topic=36313.msg1302018#msg1302018 Post by RotoSequence showing thrust & temperature vs time curves.]</ref>		#The thrust response is instantaneous while the thermal response is not.<ref>[http://forum.nasaspaceflight.com/index.php?topic=36313.msg1302018#msg1302018 Post by RotoSequence showing thrust & temperature vs time curves.]</ref>
	# ~~What about~~ [http://forum.nasaspaceflight.com/index.php?topic=36313.msg1370616#msg1370616 ~~this~~ paper by @Rodal]?		#Any thermal response is too small in magnitude.<ref>[http://forum.nasaspaceflight.com/index.php?topic=36313.msg1370616#msg1370616 Forum post referencing paper by @Rodal]</ref>

	== References ==		== References ==
	<references />		<references />

Saucyjack: Added link to @Rodal's paper

2015-05-06T22:02:14Z

Added link to @Rodal's paper

← Older revision		Revision as of 15:02, 6 May 2015
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	== Evidence Against ==		== Evidence Against ==
	#The thrust response is instantaneous while the thermal response is not.<ref>[http://forum.nasaspaceflight.com/index.php?topic=36313.msg1302018#msg1302018 Post by RotoSequence showing thrust & temperature vs time curves.]</ref>		#The thrust response is instantaneous while the thermal response is not.<ref>[http://forum.nasaspaceflight.com/index.php?topic=36313.msg1302018#msg1302018 Post by RotoSequence showing thrust & temperature vs time curves.]</ref>
			# What about [http://forum.nasaspaceflight.com/index.php?topic=36313.msg1370616#msg1370616 this paper by @Rodal]?

	== References ==		== References ==
	<references />		<references />

MazonDel: Pushed Thermal Effects page into new template and added links.

2015-05-06T18:54:46Z

Pushed Thermal Effects page into new template and added links.

← Older revision		Revision as of 11:54, 6 May 2015
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	Insert image from Reply #7 (RotoSequence) concerning the thermister data from the PZT Mach Effect Thruster from page 1.		Insert image from Reply #7 (RotoSequence) concerning the thermister data from the PZT Mach Effect Thruster from page 1.

	== ~~Links~~ ==		== Status ==
			A quick summary of the current arguments for this interpretation compared with the evidence and arguments against it.

			{\| class="wikitable"
			! style="text-align:left;"\|For \|\|Against \|\|Description
			\|-
			\| \|\| \|\|
			\|-
			\| \|\| \|\|
			\|}

			== Evidence For ==
			#Example For
			#Second Ex

			== Evidence Against ==
			#The thrust response is instantaneous while the thermal response is not.<ref>[http://forum.nasaspaceflight.com/index.php?topic=36313.msg1302018#msg1302018 Post by RotoSequence showing thrust & temperature vs time curves.]</ref>

			== References ==
			<references />

MazonDel: Note to add an image, I'm not sure how to do this just yet.

2015-05-05T15:14:11Z

Note to add an image, I'm not sure how to do this just yet.

← Older revision		Revision as of 08:14, 5 May 2015
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	One common theorized source of the anomalous thrust is that thermal effects endemic to the structure or components of the activated drive may alter the center of mass or otherwise influence the thrust reading.		One common theorized source of the anomalous thrust is that thermal effects endemic to the structure or components of the activated drive may alter the center of mass or otherwise influence the thrust reading.

			Insert image from Reply #7 (RotoSequence) concerning the thermister data from the PZT Mach Effect Thruster from page 1.

	== Links ==		== Links ==

MazonDel: Adding links section.

2015-05-05T15:10:49Z

Adding links section.

← Older revision		Revision as of 08:10, 5 May 2015
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	One common theorized source of the anomalous thrust is that thermal effects endemic to the structure or components of the activated drive may alter the center of mass or otherwise influence the thrust reading.		One common theorized source of the anomalous thrust is that thermal effects endemic to the structure or components of the activated drive may alter the center of mass or otherwise influence the thrust reading.

			== Links ==

MazonDel: Created page with "One common theorized source of the anomalous thrust is that thermal effects endemic to the structure or components of the activated drive may alter the center of mass or other..."

2015-05-05T15:09:18Z

Created page with "One common theorized source of the anomalous thrust is that thermal effects endemic to the structure or components of the activated drive may alter the center of mass or other..."

New page

One common theorized source of the anomalous thrust is that thermal effects endemic to the structure or components of the activated drive may alter the center of mass or otherwise influence the thrust reading.