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La Pinta HLLV
FunctionManned Lunar and Martian heavy lift launch vehicle
ManufacturerStages 1 & 3: Boeing
Stage 2: Grumman
Stages 4 & 5: TBD
Country of origin United States
Size
HeightTBC
Diameter~25 m
MassTBC
Stages5 (excluding Boosters)
Associated rockets
FamilyPinta
ComparableAtlas V Heavy, Ares V, Saturn V, Energia
Launch history
StatusIn development
Launch sitesLC-19
Total launches0
First flight~2031
Boosters - Delta IV CBC
No. boosters8
Engines1 RS-68
Thrust663,000 lbf
Burn time4 boosters ignite at liftoff, burn for 75 sec. then jettison, 4 boosters ignite at T+45 sec., burn for 45 sec. then jettison
PropellantLH2 / LOX
First stage
Engines12 Rocketdyne F-1A
Thrust24,447,761 lbf
Burn time165 sec.
PropellantRP-1 / LOX
Second stage
Engines10 Aerojet LR-87
Thrust4,300,000 lbf
Burn time475 sec.
PropellantRP-1 / LOX
Third stage
Engines8 Rocketdyne J-2X
Thrust1,992,000 lbf
Burn time
  • Orbit Insertation: 180 sec.
    *Trans Lunar Injection: 335 sec.
PropellantLH2 / LOX
Fourth stage
EnginesHyperdrive
ThrustTBC
Burn timeTBC
PropellantTBD
Fifth stage - RTE (Return to Earth)
EnginesHyperdrive
ThrustTBC
Burn timeTBC
PropellantTBD