2009 POKER FLAT RESEARCH RANGE LAUNCH SCHEDULE
Dates *	No.	Night / Day	Vehicle	Agency	Experimenter	Experiment	Zone*	Pad	Req'd	Launched?	Date Launched
Jan. 12-Feb.5, 2009	1	N	Black Brant IX 36.242UE	NASA	Bounds/ Univ. of Iowa	Plasma Physics	1N, 1S, 2,3,4		TBD
Jan. 12-Feb.5, 2009	1	N	Black Brant V 21.129UE	NASA	Bounds/ Univ. of Iowa	Plasma Physics	1N, 1S, 2,3,4		TBD
Jan. 10-Feb.5, 2009	1	N	Orion 30.076UE	NASA	Hawkins/ Univ. of Alaska(SRP)	Plasma Physics	1N, 1S, 2		TBD
Feb. 12-March 3, 2009	1	N	Black Brant XII 40.023UE	NASA	Lynch/ Dartmouth College	Plasma Physics	1N, 1S, 2,3,4		TBD
Feb. 12-March 3, 2009	1	N	Terrier Orion 41.076UE	NASA	Lehmacher/ Clemson	Plasma Physics	1N, 1S, 2,3,4		TBD
Feb. 12-March 3, 2009	1	N	Terrier Orion 41.077UE	NASA	Lehmacher/ Clemson	Plasma Physics	1N, 1S, 2,3,4		TBD
Feb. 12-March 3, 2009	1	N	Terrier Orion 41.078UE	NASA	Lehmacher/ Clemson	Plasma Physics	1N, 1S, 2,3,4		TBD
Feb. 12-March 3, 2009	1	N	Terrier Orion 41.079UE	NASA	Lehmacher/ Clemson	Plasma Physics	1N, 1S, 2,3,4		TBD
January Window times are from 8 PM - 2 AM AST; February Window times are from 7 PM - 1 AM AST; March 8-24, 2009 Backup Window
* Dates, Zones and Pad assignments are for planning purposes only and are subject to change without notice up to 30 days prior to launch.

General Information

Launch Timing

Most launches have a launch window which may be days or weeks long. The launch(es) may take place at any time during the window, depending on logistical, geophysical, weather, and other considerations. It is rarely possible to predict the exact time at which a given rocket will be launched. Launches are usually at night for auroral studies, but some daytime launches are performed for other types of research.

Mission Numbering

Dates	No.	Night / Day	Vehicle	Agency	Experimenter	Experiment	Zone	Pad	Req'd	Launched?	Date Launched
Feb. 18-April 7, 2003	1	N	Terrier-Orion 41.034 UE	NASA	Conde/ Univ. of Alaska	Plasma Physics	1N, 1S, 2,3,	2	NO		12:50 AM, March 25, 2003
Feb. 18-April 7, 2003	1	N	Black Brant X 35.034 UE	NASA	Conde/ Univ. of Alaska	Plasma Physics	1N, 1S, 2,3	3	NO		1:09 AM, March 25, 2003

In the vehicle column of the table above, an alpha-numeric mission code follows the rocket motor(s) designation, eg. "Terrier-Orion 41.034 UE". The first number in the code identifies the the rocket motor(s). In the case of our example above, 41 corresponds to Terrier-Orion. The following table will help you decode motor designations. Hyphenated motor names designates multi-stage rockets with two or more different rocket motors.

Numbering System for Rockets

1 - Aerobee 100	11 - Argo D-8 Journeyman	21 - Black Brant VB/C	31 - Nike-Hawk (Orion)
2 - Arcon	12 - Special Vehicles	22 - Black Brant IIIB	32 - Nike-Javelin
3 - Nike-Asp	13 - Aerobee 170	23 - Astrobee D	33 - Taurus-Orion
4 - Aerobee 150/150A	14 - Nike-Apachev	24 - Aries	34 - Taurus-Tomahawk
5 - Iris	15 - Arcas	25 - Astrobee F	35 - Black Brant X
6 - Aerobee 300	16 - Astrobee 1500	26 - Aerobee 200	36 - Black Brant IX
7 - Argo E-5	17 - Aerobee 350	27 - Nike-Black Brant V	37 - Viper-Dart
8 - Argo D-4 Javelin	18 - Nike-Tomahawk	28 - Nike-Malemute	38 - Taurus-Nike-Tomahawk
9 - Skylark	19 - Black Brant IV	29 - Terrier-Malemute	39 - Black Brant XI
10 - Nike-Cajun	20 - Bullpup-Cajun	30 - Hawk (Orion)	40 - Black Brant XII
			41 - Terrier-Orion

The second number of our example, i.e. 034 is a sequential flight identification number assignment for the year. The letters UE in our example, identify the agency and discipline responsible for the flight -- a University (University of Alaska, Fairbanks) conducting research in Plasma Physics. The following table will allow you to decode the two letter identifier.

A - Government agency other than N or D (below)
C - Industrial corporation
D - Department of Defense
G - Goddard Space Flight Center
I - International
N - NASA Center other than G or W
U - College or university
W - Wallops Flight Facility

E - Plasma Physics
G - Galactic Astronomy
H - High-energy Astrophysics
L - Planetary Atmospheres
P - Special Projects
S - Solar Physics
T - Test and Support
U - Upper Atmosphere Research

As one would expect, the size of the rocket motor limits the weight and size of the instrument payload sent aloft, the rocket's altitude at apogee, or the duration of flight through a particular region of the thermosphere. Another weight consideration is a parachute recovery system. So as with all things, there is a cost-benefit calculation involved when planning a mission. You wouldn't want to use an Aries motor when an Orion(Hawk) will do the job. The following table gives parameters of typical sounding rocket motors.

Typical Motors used for Sounding Rockets

Small

Intermediate

Large

Super Arcas

Single stage;
2.5-2.75 m long; 37.5 kg without payload;
Carries 4-8 kg payload up to 100 km altitude;
Typical flight lasts 5 minutes;
Impacts 60-70 km from launch pad.

Orion (Hawk)

Single stage;
4.6-5.3 m long; 418 kg without payload;
Carries 38 kg payload up to 88 km altitude;
Carries 68 kg payload up to 71 km altitude;
Typical flight lasts 5 minutes;
Impacts 25-50 km from launch pad.

Black Brant V

Single stage;
VB version had three fins, VC version had four fins;
9-11 m long; 1265 kg without payload;
Carries 180 kg payload up to 290 km altitude;
Carries 450 kg payload up to 140 km altitude;
Typical flight lasts 10-15 minutes;
Impacts 80-200 km from launch pad.

Nike-Orion

Two stage;
8.1-8.8 m long; 1034 kg without payload;
Carries 68 kg payload up to 190 km altitude;
Carries 204 kg payload up to 60 km altitude;
Typical flight lasts 5-10 minutes;
Impacts 30-120 km from launch pad.

Nike-Tomahawk

Two stage;
9-10.3 m long; 861 kg without payload;
Carries 45 kg payload up to 370 km altitude;
Carries 115 kg payload up to 215 km altitude;
Typical flight lasts up to 10 minutes;
Impacts 150-300 km from launch pad.

Taurus-Tomahawk

Two stage;
9.7-10.1 m long; 1608 kg without payload;
Carries 27 kg payload up to 590 km altitude;
Carries 59 kg payload up to 490 km altitude;
Typical flight lasts about 10 minutes;
Impacts 250-400 km from launch pad.

Taurus-Orion

Two stage;
9-11.7 m long; 1789 kg without payload;
Carries 68 kg payload up to 260 km altitude;
Carries 227 kg payload up to 140 km altitude;
Typical flight lasts about 10 minutes;
Impacts 60-150 km from launch pad.

Terrier-Malamute

Two stage;
10-12.6 m long; 1472 kg without payload;
Carries 90 kg payload up to 650 km altitude;
Carries 180 kg payload up to 420 km altitude;
Typical flight lasts about 10 minutes;
Impacts 200-300 km from launch pad.

Aries

Single stage (largest in use), guided rocket;
7.5-11.4 m long; 5443 kg without payload;
Carries 907 kg payload up to 500 km altitude;
Carries 1770 kg payload up to 225 km altitude;
Typical flight lasts about 10 minutes.

Nike-Black Brant VB

Two stage;
Up to 14 m long; 1881 kg without payload;
Carries 136 kg payload up to 430 km altitude;
Carries 408 kg payload up to 230 km altitude;
Typical flight lasts 6-18 minutes;
Impacts 100-300 km from launch pad.

Black Brant IX

Two stage;
Up to 13.6 m long; 2102 kg without payload;
Carries 159 kg payload up to 540 km altitude;
Carries 500 kg payload up to 230 km altitude;
Typical flight lasts about 10 minutes;
Impacts 50-150 km from launch pad

Taurus-Nike-Tomahawk

Three stage;
13-15.3 m long; 2234 kg without payload;
Carries 32 kg payload up to 700 km altitude;
Carries 125 kg payload up to 400 km altitude;
Typical flight lasts up to 15 minutes;
Impacts 180-400 km from launch pad

Flight Zones

The flight zone designation corresponds to an area on this map.

Click here for a short launch video (370K MPEG file).

For more information, please contact the Geophysical Institute Public Information Office at (907) 474-7558, or via e-mail at info@gi.alaska.edu.

Updated Fall 2008