Merge branch 'master' of ssh://git.gag.com/scm/git/web/altusmetrum

[web/altusmetrum] / MicroPeak / index.mdwn

diff --git a/MicroPeak/index.mdwn b/MicroPeak/index.mdwn
index b6fecd362ecfae6cfd4ea3aa75cd02de19ebaa00..05e432e8d41581972884529481abe26d7bc90d49 100644 (file)
--- a/MicroPeak/index.mdwn
+++ b/MicroPeak/index.mdwn
@@ -6,12 +6,12 @@
 Micropeak is a peak-recording barometric altimeter for precision model
 rocketry altitude measurements.
 
-<a href="v0.1/micropeak-dime.jpg"><img
-src="v0.1/micropeak-dime-640.jpg"></a>
+<a href="v1.0/micropeak-dime.jpg"><img
+src="v1.0/micropeak-dime-640.jpg"></a>
 
 Production units are available from the
 [Garbee and Garbee](http://auric.gag.com/index.php?route=product/product&product_id=80) 
-web store 
+web store and [Apogee Components](http://www.apogeerockets.com/Electronics_Payloads/Altimeters/MicroPeak_Altimeter)
 
 ## Documentation ##
 
@@ -39,14 +39,14 @@ The CR1025 battery holder is mounted on the back side of the board, so there are
 MicroPeak includes an integrated battery holder on the back side of
 the circuit board.
 
-<a href="v0.1/micro-peak-back.jpg"><img
-src="v0.1/micro-peak-back-640.jpg"></a>
+<a href="v1.0/micropeak-back.jpg"><img
+src="v1.0/micropeak-back-640.jpg"></a>
 
 ## Developer View ##
 
 Here's a close-up view of the hardware
 
-<a href="v0.1/micropeak.jpg"><img src="v0.1/micropeak-640.jpg"></a>
+<a href="v1.0/micropeak.jpg"><img src="v1.0/micropeak-640.jpg"></a>
 
  * Hardware Features
        * [ATMEL ATtiny85](http://www.atmel.com/devices/attiny85.aspx) Microcontroller
@@ -60,13 +60,14 @@ Here's a close-up view of the hardware
                * Factory calibrated.
        * CR1025 Lithium Battery
                * 30mAh. Runs MicroPeak for more than 40 hours on the pad or in flight
+       * [OSRAM LO T67K](http://catalog.osram-os.com/catalogue/catalogue.do?favOid=000000000002269f00090023&act=showBookmark) orange LED
        * Standard 6-pin AVR programming interface.
 
  * Software Features
        * Written in C
        * Samples pressure every 96ms
        * Delay 30s after power-on to finish airframe prep
-       * Detect boost with 20m altitude change
+       * Detect boost with 10m altitude change
        * Exponential averaging filter to minimize transient effects.
 
  * Tools Used