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Introduction
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<table>
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<h2><a name="What is the PSAS?"></a> What is the PSAS? </h2>
<p> The Portland State Aerospace Society (PSAS) is a non-profit (501c3) aerospace project at Portland State University in Portland, Oregon. The group consists of undergraduate and graduate students, faculty and staff of PSU, and local community members- ranging from high school students to engineers in industry- who are interested in aerospace engineering. </p>
<p> The PSAS is based out of the College of Engineering and Computer Science at PSU, and has members and advisors in the Electrical and Computer Engineering, Computer Science and Mechanical Engineering departments. </p>
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- <p>[[bw_group_10-2000.jpg]]</p>
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<h2><a name="What does the PSAS do?"></a> What does the PSAS do? </h2>
<p> Our vision statement &ndash; or long term goal &ndash; is to &ldquo;put nanosatellites into orbit&rdquo;. That&rsquo;s an absurdly hard undertaking when you consider the technical, logistical and financial problems involved. So although we may never get there, having this goal allows us to ask the question, &ldquo;what&rsquo;s the first step in the process?&rdquo; </p>
<p> We decided that the first step towards orbiting nanosatellites is to develop an inexpensive, highly modular and actively guided sounding rocket. Sounding rockets are small to medium-sized rockets that are &quot;suborbital&quot; - meaning they can reach extreme altitudes, but then fall down back to the Earth (i.e., they don&#39;t go into orbit). Sounding rockets are useful for scientific research in such fields as astronomy, earth science, materials science, and of course, in engineering. </p>
<p> Our rockets fall into the class of &ldquo;amateur rocketry&rdquo; &ndash; smaller than commercial rockets, larger than model rockets. We certainly have not build the biggest or highest altitude amateur rocket, but we do hope that we&rsquo;re building one of the most sophisticated. </p>
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@@ -52,59 +36,26 @@ We're focusing in four main areas:
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- <p><strong>Advanced Avionics:</strong> Avionics are the computer &quot;brains&quot; of the rocket. We&#39;re trying to be one of the first amateur groups in the world to make an actively guided rocket &ndash; i.e., a rocket that is autonomously guided by an onboard computer. Technically speaking, we&#39;re hoping to build an amateur DGPS-aided inertial navigation system. </p>
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- <p><img align="center" height=319 src="/psas/Current_project/LV-1/Payload/Resources/FC_Intro.jpg" width=320></p>
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+ <td><strong>Advanced Avionics:</strong> Avionics are the computer &quot;brains&quot; of the rocket. We&#39;re trying to be one of the first amateur groups in the world to make an actively guided rocket &ndash; i.e., a rocket that is autonomously guided by an onboard computer. Technically speaking, we&#39;re hoping to build an amateur DGPS-aided inertial navigation system. </td>
+ <td><img align="center" height=319 src="/psas/Current_project/LV-1/Payload/Resources/FC_Intro.jpg" width=320></td>
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- <p><strong>Adaptable Airframes:</strong> We&#39;re working on modular airframe sections to reduce the weight and cost of the rocket while increasing adaptability. Airframe sections are easily swappable, as are the fins and skin. Technically speaking, we&#39;re hoping to push our mass fraction up as high as possible - beyond 60% for a single stage vehicle - while still maintaining robustness. </p>
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- <p>[[smalllv2airframe.jpg]]</p>
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+ <td><strong>Adaptable Airframes:</strong> We&#39;re working on modular airframe sections to reduce the weight and cost of the rocket while increasing adaptability. Airframe sections are easily swappable, as are the fins and skin. Technically speaking, we&#39;re hoping to push our mass fraction up as high as possible - beyond 60% for a single stage vehicle - while still maintaining robustness. </td>
+ <td>[[smalllv2airframe.jpg]]</td>
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- <p><strong>High Energy Motors:</strong> Given the number of launches we would like to do in the future, we are developing our own solid-fuel motors. Technically speaking, we&rsquo;re using an industry standard Ammonium Perchlorate/Aluminum composite formula to produces motors in the 10K-60K N-sec range. In the future we&#39;ll move to hybrids for their safety and controllability. </p>
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- <p>[[Smallo.jpg]]</p>
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+ <td><strong>High Energy Motors:</strong> Given the number of launches we would like to do in the future, we are developing our own solid-fuel motors. Technically speaking, we&rsquo;re using an industry standard Ammonium Perchlorate/Aluminum composite formula to produces motors in the 10K-60K N-sec range. In the future we&#39;ll move to hybrids for their safety and controllability. </td>
+ <td>[[Smallo.jpg]]</td>
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- <p><strong>Mobile Ground Systems:</strong> Since our launch sites and times are dictated by the FAA and the whims of the weather, our ground systems are designed to be as mobile and flexible as possible. The ground systems include the launch tower, launch control module, radio systems, computers, and logistical equipment. </p>
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- <p>[[SmallLaunchTower.jpg]]</p>
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+ <td><strong>Mobile Ground Systems:</strong> Since our launch sites and times are dictated by the FAA and the whims of the weather, our ground systems are designed to be as mobile and flexible as possible. The ground systems include the launch tower, launch control module, radio systems, computers, and logistical equipment. </td>
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@@ -114,46 +65,20 @@ We've successfully launched three rockets so far:
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- <p><a href="/psas/Current_project/LV-0/Project_Navigation_LV-0.html">Launch Vehicle No. 0</a> (LV0) was our first launch in June of 1998 to 366m (1,200ft). It was our first rocket and a proof of concept for some of our radio systems, including real-time broadcast video. It was a great introduction to amateur rocketry for many of us <a href="/psas/Schedule/Monroe6_7_98/6_7_98.html">(Launch Results and Videos)</a>. </p>
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- <p>[[SmallLV0.jpg]]</p>
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+ <td><a href="/psas/Current_project/LV-0/Project_Navigation_LV-0.html">Launch Vehicle No. 0</a> (LV0) was our first launch in June of 1998 to 366m (1,200ft). It was our first rocket and a proof of concept for some of our radio systems, including real-time broadcast video. It was a great introduction to amateur rocketry for many of us <a href="/psas/Schedule/Monroe6_7_98/6_7_98.html">(Launch Results and Videos)</a>. </td>
+ <td>[[SmallLV0.jpg]]</td>
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- <p><a href="/psas/Current_project/LV-1/Lv1menu.html">Launch Vehicle No. 1</a> (LV1) was our next rocket that flew in April of 1999 to 3.6km (12,000ft). It was our proof of concept for several new systems, including a emergency uplink system, inertial sensors, and a more advanced telemetry system <a href="/psas/Schedule/Bend4_11_99/Bend4_11_99.html">(Launch Results and Videos)</a>. </p>
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- <p>[[WheresLV1.jpg]]</p>
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+ <td><a href="/psas/Current_project/LV-1/Lv1menu.html">Launch Vehicle No. 1</a> (LV1) was our next rocket that flew in April of 1999 to 3.6km (12,000ft). It was our proof of concept for several new systems, including a emergency uplink system, inertial sensors, and a more advanced telemetry system <a href="/psas/Schedule/Bend4_11_99/Bend4_11_99.html">(Launch Results and Videos)</a>. </td>
+ <td>[[WheresLV1.jpg]]</td>
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- <p><font color="#009900">Launch Vehicle No. 1b</font> (LV1b) used the same airframe as LV1 and flew in October of 2000 to 3.53km (11,600ft). The major change was a major upgrade to the avionics system: we added a GPS, upgraded the flight computer and improved the inertial sensors. This was our step towards the the electronics system necessary to do active guidance <a href="/psas/Schedule/Bend10_7_00/Bend10_7_00html.html">(Launch Results and Videos)</a>. </p>
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- <p>[[Lv1bIMU.jpg]]</p>
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+ <td><font color="#009900">Launch Vehicle No. 1b</font> (LV1b) used the same airframe as LV1 and flew in October of 2000 to 3.53km (11,600ft). The major change was a major upgrade to the avionics system: we added a GPS, upgraded the flight computer and improved the inertial sensors. This was our step towards the the electronics system necessary to do active guidance <a href="/psas/Schedule/Bend10_7_00/Bend10_7_00html.html">(Launch Results and Videos)</a>. </td>
+ <td>[[Lv1bIMU.jpg]]</td>
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@@ -162,18 +87,10 @@ We also try and reach out to the community as much as possible. We're a regular
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<h2><a name="What are your current projects?"></a> What are your current projects? </h2>
<p> We&#39;re currently working on the next generation vehicle, called <a href="/psas/Current_project/LV-2/LV2menu.html">Launch Vehicle No. 2</a> (LV2) which should be launched during the summer of 2002. It has a projected altitude of 21km (70,000ft), has an advanced avionics system which will be the basis for our active guidance system, a modular airframe system, and perhaps most importantly, builds on everything we&#39;ve learned from the last three rockets. LV2 is partially funded from a $10,000 grant from the NASA Space Grant Program. </p>
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<h2><a name="Can I get involved?"></a> Can I get involved? </h2>
<p> Absolutely! We need the help! We&#39;re looking for anyone who is interested in rocketry or engineering. There are thousands of problems to tackle, ranging from control theory analysis to airframe design to computer programming to logistics support. [[Contacts]], or drop in on [[Schedule]], and we&#39;ll introduce you to the project and let you decide where you want to fit in! </p>
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