The ThunderPack Revision-2, Generation-2 (R2G2), is the current enhanced rocketbelt design produced by Thunderbolt Aerosystems between 2004 and 2006. This model can be manufactured to operate on either dual-fuel mode, as its predecessor TP-R1G2 and it can utilize specially promoted hydrogen peroxide (PERTOL) or standard High Test Peroxide, or can be ordered operating in monopropellant mode, utilizing only specially promoted hydrogen peroxide (PERTOL) or standard High Test Peroxide

The TP-R2G2M (monopropellant mode) is the flagship of Thunderbolt Aerosystems and has been tested with flight durations ranging between 35 to 45 seconds with a standard pilot weight of 160 lbs. These actual flight durations include reserve fuel capacity (typically, 5 to 10 seconds reserve is necessary for average safe landings) and assumes an ascension rate of 5 feet per second. Flight times vary on fuel load, pilot plus payload weight and variability of acceleration after take-off.

The model TP-R2G2D (dual-fuel mode), has been bench tested for a potential flight duration of 75 seconds with a standard pilot weight of 160 lbs plus 20 lbs payload (180 lbs gross weight). This anticipated flight duration does not take into account the reserve fuel capacity (typically, 5 to 10 seconds reserve is necessary for average safe landings) and assumes an ascension rate of 5 feet per second. Flight times vary on fuel load, pilot plus payload weight and variability of acceleration after take-off.

Both current models TP-R2G2M and TP-R2G2D have a maximum gross (pilot plus payload) take-off weight of 340 lbs and thrust can be adjusted with a simple control mechanism on the ThunderPacks, to match the pilots’ take-off weight. Flight duration and take-off weight are inversely proportional (higher pilot+payload weight = shorter flight times and range).

R2G2
ThunderPack Model TP-R2G2 on its stand prior a tether test
   TECHNICAL SPECIFICATION
  H²O² ONLY H²O² + JP4
Takeoff weight, lbs 350 350
Empty (dry) weight, lbs 72 80
Pilot  + Payload, lbs
Pilot
Payload
180
160
20
180
160
20
Total Fuel, lbs
H²O²
JP4 (kerosene)


92


92

Range, feet 1,805 3,650
Speed, mph 65+ 75+
Endurance, seconds 45 75
Type of Fuel 90 – 92% H²O² 90 – 92% H²O² + JP4-JP5-JP10
Propellant Isp, lb/lb/sec 133 181
Total Thrust, lbs-force 340 380
C-Star Efficiency > 95% > 95%
Exit Pressure, psig 350 370
Engine Life, seconds 11,500 10,800
Mean Time To Repair, hrs 2.8 2.5
Flights Before Maintenance 350 300
Price, US Dollars $ CALL $ CALL
Delivery Time, ARO days 150 150
Availability NOW SUMMER 2009