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Saturn I Block II

Saturn I Block II was the operational two-stage Saturn I configuration flown by SA-5, SA-6, SA-7, SA-9, SA-8, and SA-10. It paired the eight-engine S-I first stage with a live six-engine S-IV upper stage, achieving orbit with boilerplate Apollo spacecraft and, on the final three flights, Pegasus micrometeoroid satellites.

Identity

Aliases
Saturn C-1 Block II
Family Name
Saturn I
Full Name
Saturn I Block II
Reusability
expendable
Slug
saturn-i-block-ii
Status
retired
Type
rocket
Variant Name
Block II

Details

Description
Saturn I Block II was the operational two-stage Saturn I configuration flown by SA-5, SA-6, SA-7, SA-9, SA-8, and SA-10. It paired the eight-engine S-I first stage with a live six-engine S-IV upper stage, achieving orbit with boilerplate Apollo spacecraft and, on the final three flights, Pegasus micrometeoroid satellites.
Diameter M
6.52
Engines
  • Count
    8
    Name
    H-1
    Placement
    core
  • Count
    6
    Name
    RL10-A-3
    Placement
    upper
First Flight Year
1,964
Height M
57.3
Last Flight Year
1,965
Liftoff Mass Kg
512,000
Manufacturer Id
vh76vnx3yy1vy23j7zc3wk80wx7nhx5f
Operator Id
vh76vnx3yy1vy23j7zc3wk80wx7nhx5f
Parent Vehicle Family Id
nd7w4ck2ytprw5jw7215jv26r18agw4v
Payload Capacity Kg
Leo
9,000
Stages Count
2
Strap On Boosters Count
0

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Creation Time
7/14/2026, 8:31:06 AM
Updated Time
7/14/2026, 8:31:06 AM