From cb713565a2bf301288c2488466e29473d6435c5a Mon Sep 17 00:00:00 2001 From: Lars Seimetz Date: Tue, 23 Jul 2024 14:05:37 +0000 Subject: [PATCH 1/3] Update on Overleaf. --- cau-ath-er_i1-0/report.tex | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/cau-ath-er_i1-0/report.tex b/cau-ath-er_i1-0/report.tex index 8aa40e4..ed2b776 100644 --- a/cau-ath-er_i1-0/report.tex +++ b/cau-ath-er_i1-0/report.tex @@ -134,7 +134,7 @@ The proposed sensor design of the \acs{AHEPaM} is sketched in Fig. \ref{fig:tele Key properties such as mass, power, volume, etc.\,of the AHEPaM developed under this contract are given in Tab.~\ref{tab:key-properties}. One can easily see that \acs{AHEPaM} is indeed very compact and is close to fulfilling the original measurement requirements. It is also clear that it is probably not possible to satisfy all the measurement requirements within the resource allocations foreseen for \acs{AHEPaM}. This is one of the lessons learned from the work performed under this contract. The measurement capabilities of \acs{AHEPaM} are summarized in Tab.~\ref{tab:AHEPaM-data-products} and discussed in more detail in Sec.~\ref{sec:performance}. -The mechanical, thermal, and electrical interfaces of \acs{AHEPaM} with the \acs{ATHENA} spacecraft were designed to be as straightforward as possible. Mechanically, \acs{AHEPaM} is bolted ... {\bf Lars Seimetz to write a brief description, incl. UPM results}. \acs{AHEPaM} is thermally isolated from the spacecraft ... {\bf Lars Seimetz: brief description also of UPM results}. \acs{AHEPaM} requires standard {\bf XYZ} voltages, {\bf Björn}, and communicates with \acs{ATHENA} via the {\bf XYZ} interface {\bf Björn}. +The mechanical, thermal, and electrical interfaces of \acs{AHEPaM} with the \acs{ATHENA} spacecraft were designed to be as straightforward as possible. Mechanically, \acs{AHEPaM} is bolted ... {\gree Lars Seimetz to write a brief description, incl. UPM results}. \acs{AHEPaM} is thermally isolated from the spacecraft ... {\bf Lars Seimetz: brief description also of UPM results}. \acs{AHEPaM} requires standard {\bf XYZ} voltages, {\bf Björn}, and communicates with \acs{ATHENA} via the {\bf XYZ} interface {\bf Björn}. The design of \acs{AHEPaM} that resulted from this study is shown in Fig.~\ref{fig:basic-arrangement}. The left-hand figure (Fig.~\ref{fig:ahepam-wo-cover}) shows the particle telescope that was shown in detail in Fig.~\ref{fig:AHEPaM-concept} in pale blue mounted to the top of the electronics box (\acs{EBox}), shown in dark green. This chassis provides the structural support for the particle telescope and provides shielded routing of the cables which carry the analog signals from the sensor head to the \acs{EBox}. From 77f65c9c11c8965a9fec0d95709f423add8e5c75 Mon Sep 17 00:00:00 2001 From: Lars Seimetz Date: Tue, 23 Jul 2024 14:05:44 +0000 Subject: [PATCH 2/3] Update on Overleaf. --- cau-ath-er_i1-0/report.tex | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/cau-ath-er_i1-0/report.tex b/cau-ath-er_i1-0/report.tex index ed2b776..bdac411 100644 --- a/cau-ath-er_i1-0/report.tex +++ b/cau-ath-er_i1-0/report.tex @@ -134,7 +134,7 @@ The proposed sensor design of the \acs{AHEPaM} is sketched in Fig. \ref{fig:tele Key properties such as mass, power, volume, etc.\,of the AHEPaM developed under this contract are given in Tab.~\ref{tab:key-properties}. One can easily see that \acs{AHEPaM} is indeed very compact and is close to fulfilling the original measurement requirements. It is also clear that it is probably not possible to satisfy all the measurement requirements within the resource allocations foreseen for \acs{AHEPaM}. This is one of the lessons learned from the work performed under this contract. The measurement capabilities of \acs{AHEPaM} are summarized in Tab.~\ref{tab:AHEPaM-data-products} and discussed in more detail in Sec.~\ref{sec:performance}. -The mechanical, thermal, and electrical interfaces of \acs{AHEPaM} with the \acs{ATHENA} spacecraft were designed to be as straightforward as possible. Mechanically, \acs{AHEPaM} is bolted ... {\gree Lars Seimetz to write a brief description, incl. UPM results}. \acs{AHEPaM} is thermally isolated from the spacecraft ... {\bf Lars Seimetz: brief description also of UPM results}. \acs{AHEPaM} requires standard {\bf XYZ} voltages, {\bf Björn}, and communicates with \acs{ATHENA} via the {\bf XYZ} interface {\bf Björn}. +The mechanical, thermal, and electrical interfaces of \acs{AHEPaM} with the \acs{ATHENA} spacecraft were designed to be as straightforward as possible. Mechanically, \acs{AHEPaM} is bolted ... {\colo Lars Seimetz to write a brief description, incl. UPM results}. \acs{AHEPaM} is thermally isolated from the spacecraft ... {\bf Lars Seimetz: brief description also of UPM results}. \acs{AHEPaM} requires standard {\bf XYZ} voltages, {\bf Björn}, and communicates with \acs{ATHENA} via the {\bf XYZ} interface {\bf Björn}. The design of \acs{AHEPaM} that resulted from this study is shown in Fig.~\ref{fig:basic-arrangement}. The left-hand figure (Fig.~\ref{fig:ahepam-wo-cover}) shows the particle telescope that was shown in detail in Fig.~\ref{fig:AHEPaM-concept} in pale blue mounted to the top of the electronics box (\acs{EBox}), shown in dark green. This chassis provides the structural support for the particle telescope and provides shielded routing of the cables which carry the analog signals from the sensor head to the \acs{EBox}. From fd7b491ffcf49fed980b03b2299f5cbb8ff11e7b Mon Sep 17 00:00:00 2001 From: Lars Seimetz Date: Tue, 23 Jul 2024 14:18:15 +0000 Subject: [PATCH 3/3] Update on Overleaf. --- cau-ath-er_i1-0/report.tex | 2 +- 1 file changed, 1 insertion(+), 1 deletion(-) diff --git a/cau-ath-er_i1-0/report.tex b/cau-ath-er_i1-0/report.tex index bdac411..a970b0a 100644 --- a/cau-ath-er_i1-0/report.tex +++ b/cau-ath-er_i1-0/report.tex @@ -134,7 +134,7 @@ The proposed sensor design of the \acs{AHEPaM} is sketched in Fig. \ref{fig:tele Key properties such as mass, power, volume, etc.\,of the AHEPaM developed under this contract are given in Tab.~\ref{tab:key-properties}. One can easily see that \acs{AHEPaM} is indeed very compact and is close to fulfilling the original measurement requirements. It is also clear that it is probably not possible to satisfy all the measurement requirements within the resource allocations foreseen for \acs{AHEPaM}. This is one of the lessons learned from the work performed under this contract. The measurement capabilities of \acs{AHEPaM} are summarized in Tab.~\ref{tab:AHEPaM-data-products} and discussed in more detail in Sec.~\ref{sec:performance}. -The mechanical, thermal, and electrical interfaces of \acs{AHEPaM} with the \acs{ATHENA} spacecraft were designed to be as straightforward as possible. Mechanically, \acs{AHEPaM} is bolted ... {\colo Lars Seimetz to write a brief description, incl. UPM results}. \acs{AHEPaM} is thermally isolated from the spacecraft ... {\bf Lars Seimetz: brief description also of UPM results}. \acs{AHEPaM} requires standard {\bf XYZ} voltages, {\bf Björn}, and communicates with \acs{ATHENA} via the {\bf XYZ} interface {\bf Björn}. +The mechanical, thermal, and electrical interfaces of \acs{AHEPaM} with the \acs{ATHENA} spacecraft were designed to be as straightforward as possible. Mechanically, \acs{AHEPaM} is bolted ... \colorbox{green}{Mechanical interface andSeimetz to write a brief description, incl. UPM results more .................................}. \acs{AHEPaM} is thermally isolated from the spacecraft ... {\bf Lars Seimetz: brief description also of UPM results}. \acs{AHEPaM} requires standard {\bf XYZ} voltages, {\bf Björn}, and communicates with \acs{ATHENA} via the {\bf XYZ} interface {\bf Björn}. The design of \acs{AHEPaM} that resulted from this study is shown in Fig.~\ref{fig:basic-arrangement}. The left-hand figure (Fig.~\ref{fig:ahepam-wo-cover}) shows the particle telescope that was shown in detail in Fig.~\ref{fig:AHEPaM-concept} in pale blue mounted to the top of the electronics box (\acs{EBox}), shown in dark green. This chassis provides the structural support for the particle telescope and provides shielded routing of the cables which carry the analog signals from the sensor head to the \acs{EBox}.