Under "Typical Apollo Burns"
Boost to Orbit: 31,000 fps (21,136 MPH)
Speed in orbit: 25,570 fps (17,434 MPH)
Translunar injection:10,000-10,600 fps (6816-7227 MPH)
Midcourse corrections:150 fps (102 MPH)
Lunar Orbit Insertion:3,000-3,500 fps (2045-2386 MPH)
Speed in Lunar Orbit: 5348 fps (3646 MPH)
Descent orbit insertion: 140 fps (95 MPH)
Powered descent/Land: 6900 fps (4705 MPH)
Lunar launch to Orbit: 6100 fps (4159 MPH)
TransEarth Injection: 3500 fps (2386 MPH)
Midcourse Corrections: 150 fps (102 MPH)
Entry velocity: 36,000-36,300 fps (24,545 - 24,750 MPH)

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As I'd said, relative to NEO, you AT LEAST save the 6900fps powered decent and the 6100fps Lunar launch. I contend that there are many NEOs that require LESS THAN the 3500fps LOI delta V as well.

Therefore, smaller fuel loads and therefore smaller rockets can send humans to NEOs than can reach the moon, by a substantial margin. Proton class launch vehicles could likely put a hab + 2 booster/fuel rockets into LEO to reach a NEO. 3 launches.

-philw