Lightweight ExoAtmospheric Projectile (LEAP) - United States ...

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LEAP 4 TARGET LAUNCH VEHICLE I 3a Distribution of Debris for Missile Destruct Through Aries Bum r--+-- 3cr Distribution of D~>bris tor Missile Destruct During Orbus·1 Bum .--+--- 3a Distribution tor Orbus·1 Impact 30' Distribution for Aries Booster Impact 0 5 10 15 Miles · appn>ximate scale - · I LEAP ENVIRONMENTiL ASSESSMENT I 1-22 LEAP DISPERSION AREAS .WSMR Figure 70
·-·· 160' E. 165' E. 170' E. 175' E. 180' E. 20' N. 20' N. ·-·· 3o Olslrlbullon aboul Nominal Splashdown 3o Dlllrbullon of Debris lor Missile destruct up to Tlmo ol Orbua Bum (642 eec) I 3o Olstrt>ullon of Oebrb lor Missile Destruct during 2nd Stage Burn 15' N. 15' N. ·aa DlatrbuUon ol Debris lor Missile Destruct during Orbus Bum _. 8 3o Dlatri!UIIon about Nominal Splashdown 3o Dlslrlbullon ol Debris lor Missile destruct during 1st Stage Burn 10' N. ' to· N. ~ \\ ~- "' \~ \) I I () 5'N. ~------------~---------------L-~------------~--------------J 5' N. 160' E. 16!>' E. 170' E .. 175' E. tso· E. • \ LEAP ENVIRONMENTAL ASSESSMENT LEAP DISPERSION AREAS USAKA/WAKE ISLAND Figure 8
Page 1 and 2: LEAP PROGRAM ENVIRONMENTAL ASSESSME
Page 3 and 4: similar and both employ liquid hi-p
Page 5 and 6: . ., I State of New Mexico ) • Sa
Page 7 and 8: --- Pacific Ocean EBADON-~.J' 0 0
Page 9 and 10: I ) . J I been adopted (USASDC, 198
Page 11 and 12: ---------- lightning poles, pad con
Page 13 and 14: ·- _ ___....- __, - - ------ ...-
Page 15 and 16: authorizations necessary for curren
Page 17 and 18: TWO VEHICLE MISSION TWO VEHICLE MIS
Page 19 and 20: 1 LEAP 1 & 2 3c Distribution for Sh
Page 21: LEAP 4 PROBE LAUNCH VEHICLE J ) 3a
Page 25 and 26: 300 T • 523.0 REENTRY ROCKET ION
Page 27 and 28: place the target on a preprogrammed
Page 29 and 30: Three major assemblies make up the
Page 31 and 32: The LEAP launch vehicle to be launc
Page 33 and 34: I l ) Once the fluids reach USAKA,
Page 35 and 36: l I ) accordance with Safety Standi
Page 37 and 38: ( ) J ) Wake Island Launches Target
Page 39 and 40: )• ' flightweight motor cases suc
Page 41 and 42: Flight safety planning is an iterat
Page 43 and 44: j I l I 1 . in accordance with the
Page 45 and 46: 125 Recovezy and Decommissioning .,
Page 47 and 48: ] . l 1 6. match the surrounding te
Page 49 and 50: 1 • ! 2. All recovery operations
Page 51 and 52: .... .... 3 4 Boosting Solid (Orbus
Page 53 and 54: i I l . I ) LEAP target launches. T

Lightweight ExoAtmospheric Projectile (LEAP) - United States ...

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