Loki (rocket)

. It was so successful in this role that several advanced versions were developed on the basic Loki layout, including the final Super Loki.

Development

Taifun was powered by a hypergolic mixture pressure-fed into the combustion chamber. The pressure was provided by small cordite charges that were fired into the fuel tanks, in the process bursting a pair of thin diaphragms to allow the fuel and oxidizer to flow into the combustion chamber. The Germans were never able to get the engine to work reliably, and the rocket was never deployed operationally.

American efforts to further develop the system started at Bendix in 1948, after the US Army had initially studied the Taifun in 1946. One major change was to replace the warhead area with a dart-like version, which was separated from the main rocket body at engine burnout to continue on without the drag of the airframe and thereby reach higher altitudes. Like the Germans before them, Bendix had significant problems with the engine, and eventually decided to develop a solid-fuel engine based on a new elastomeric fuel from the Jet Propulsion Laboratory (JPL), starting in March 1951. The new engine was successful, and the liquid engine was abandoned in February 1952.

The first flight of a solid-fuel Loki occurred in June 1951. JPL eventually fired 3,544 at White Sands during the testing program, where it was discovered that the launch of one rocket would affect the flight path of the ones behind it, making the dispersion too large to be a useful weapon. Although this problem was studied in depth, it appeared there was no obvious solution. The Army eventually gave up on Loki in September 1955, in favour of the Nike-Ajax missile, which had recently reached operational status.

Loki specifications

* payload: 3.2 kg (dart)
* dimensions:
*: booster: 2.63 m long x 76 mm diameter
*: dart: 1.02 m long x 35 mm diameter
* weight:
*: booster: 13 kg
*: dart: 3.2 kg
* maximum height: 55 km
* maximum speed 6,275 km/h

ounding rockets

In 1955 the US Navy took many of the already-completed Loki's and replaced the explosive warhead with a chaff dispenser. These WASP rockets were fired from ships directly upward, and the chaff released at apogee where it was tracked by radar in order to accurately measure the winds aloft. The USAF also used the Loki for this role, assigning it the name XRM-82. The ONR also used the Loki in some of its Rockoon launches, lofting the Loki to high altitudes on a helium balloon before firing.

Many other Loki's were sold into the civilian market, where they became quite popular for meteorological work, referred to as the Loki-Dart. To better serve the needs in this role, a larger-diameter motor with 50% more fuel was developed in 1957, creating the Loki II, the original retroactively becoming Loki I. Other companies developed additional versions, including the Cooper Development /Marquardt Rocksonde 100 with a 100,000 ft maximum altitude and Rocksonde 200 able to reach 200,000 ft.

DC

In 1963 Space Data Corporation (SDC) formed to provide small sounding rockets to the various defence agencies. They used the meteorological rockets and created an instrument payload for the Loki in place of the chaff dispenser. The instruments consisted primarily of a thermistor to collect temperature, which was broadcast via a small radio. Altitude was tracked from the ground, by reflecting radar off the probe's "starute", a square mylar parachute and radar reflector. The SDC version was slightly heavier than the original Loki in order to improve stability during "cruise", which lowered maximum altitude by about 10,000 ft. Production of the Loki Datasonde started in 1966, and more than 20,000 were built until production ended in 1985.

The Air Force requested a version that would not require radar tracking, and SDC responded by placing a transponder in the payload. This increased payload weight, and required the starute to be enlarged, further increasing launch weight. To reach the required altitudes, SDC developed a much larger booster, which also increased overall weight and further improved stability. The resulting Super Loki first flew in 1968, and since then 9,000 have been delivered.

The Air Force Meteorologists and NASA's Observational Scientists desired higher apogees with the ROBINSphere payloads in the early 1970s. In 1972, Space Data completed the development of the 4 1/2 inch diameter Viper IIIA solid propellant rocket motor. This motor followed the design of the Super Loki nearly identically and provided apogees of ~120 km for the ROBINSphere. This higher apogee allowed for measuring the wind and atmospheric vertical profiles through the 110 - 95 km region that were unobtainable from the Super Loki boosted ROBINSphere.

A design change occurred in 1993 with a change in the elastomeric solid propellant with the more commonly available polymer, HTPB (hydroxyl terminated polybutadiene). This propellant design change occurred both in the Super Loki and the Viper IIIA.

Orbital Sciences Corporation bought SDC in 1990. The production of the Super Loki and the Viper IIIA rocket boosted meteorological payloads continued until 2001 when the product line was abandoned.

uper Loki specifications

* payload: 6 kg
* maximum height: 103 km
* takeoff thrust: 4500 lbf (18 kN)
* takeoff weight: 29 kg
* diameter: Motor 4 inch
* length: 3.16 m
* fin span: 0.20 m

References

*http://www.astronautix.com/lvs/loki.htm
*http://www.astronautix.com/lvs/suprloki.htm
*http://www.planet4589.org/space/lvdb/launch/Loki
*http://www.designation-systems.net/dusrm/app4/loki.html
*http://www.designation-systems.net/dusrm/n-1.html
*http://www.designation-systems.net/dusrm/n-5.html
*http://www.designation-systems.net/dusrm/n-8.html
*http://www.designation-systems.net/dusrm/n-10.html
*http://www.designation-systems.net/dusrm/n-11.html
*http://www.designation-systems.net/dusrm/n-12.html
*http://www.designation-systems.net/dusrm/app4/hasp.html