blackshire
02-13-2011, 07:24 PM
Hello All,
This morning I found that the Thiokol Malemute (which has been used as the upper stage of the Nike-Malemute, Terrier-Malemute, and Terrier-Improved Malemute sounding rockets for decades) was also flown at least twice as a single-stage rocket in 1976, in order to test the motor in a spinning flight regime. Below are two links to scale data and historical information on these two NASA test vehicles--as well as a color photograph of a similar U.S. Navy single-stage Malemute II (used as a radar target in a "Slugger" ballistic missile defense test) at launch in 1999 (that photograph is also attached below).
The two NASA Malemute test vehicles were launched at Sandia's Tonopah, Nevada rocket range, and they utilized an unusual recovery sequence--in each flight, three of the rocket's four fins were blown off after motor burnout to make it tumble, to facilitate recovery closer to the launch site. The one-finned spent rockets didn't tumble until they were on the descending legs of their trajectories, however, which resulted in peak altitudes of over 140 km instead of the predicted 44 km! Here are the links:
http://www.designation-systems.net/dusrm/app4/other.html
[NOTE: the Malemute photograph is near the bottom of this web site's "screen-page."]
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19780016341_1978016341.pdf
[NOTE: The Malemute general arrangement dimensioned drawing is on page 21 of this report, and a dimensioned drawing of the Malemute rocket motor in on page 14.]
I hope this material will be useful.
This morning I found that the Thiokol Malemute (which has been used as the upper stage of the Nike-Malemute, Terrier-Malemute, and Terrier-Improved Malemute sounding rockets for decades) was also flown at least twice as a single-stage rocket in 1976, in order to test the motor in a spinning flight regime. Below are two links to scale data and historical information on these two NASA test vehicles--as well as a color photograph of a similar U.S. Navy single-stage Malemute II (used as a radar target in a "Slugger" ballistic missile defense test) at launch in 1999 (that photograph is also attached below).
The two NASA Malemute test vehicles were launched at Sandia's Tonopah, Nevada rocket range, and they utilized an unusual recovery sequence--in each flight, three of the rocket's four fins were blown off after motor burnout to make it tumble, to facilitate recovery closer to the launch site. The one-finned spent rockets didn't tumble until they were on the descending legs of their trajectories, however, which resulted in peak altitudes of over 140 km instead of the predicted 44 km! Here are the links:
http://www.designation-systems.net/dusrm/app4/other.html
[NOTE: the Malemute photograph is near the bottom of this web site's "screen-page."]
http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19780016341_1978016341.pdf
[NOTE: The Malemute general arrangement dimensioned drawing is on page 21 of this report, and a dimensioned drawing of the Malemute rocket motor in on page 14.]
I hope this material will be useful.