Edge Rewrite
// HTMLRewriter · presentation

This page was redesigned at the edge.

Cloudflare fetched the original article and streamed it through HTMLRewriter to apply an entirely new visual system without rebuilding the source page.

// request.cf · coarse context

A page that knows where it met you.

Only coarse request metadata is shown. This demo does not display or persist visitor IP addresses.

Country
US
Cloudflare location
CMH
Connection
HTTP/2
Language
Not provided

Ray ID: a25439e4bcf01ef0

Jump to content

// Workers AI · dad joke modeWhy did Lockheed Saturn go to therapy? It had a lot of space to work through.

From Wikipedia, the free encyclopedia

Model 75 Saturn
General information
TypeAirliner
National originUnited States
ManufacturerLockheed Corporation
StatusScrapped
Number built2
History
First flightJune 17, 1946

The Lockheed Model 75 Saturn was a small, short-route commercial aircraft produced by the Lockheed Corporation in the mid-1940s. Lockheed announced the project on November 19, 1944.[1] The design team, led by Don Palmer, created a high-wing, twin-engine monoplane with 14 seats and a top speed of 228 mph (367 km/h). Lockheed touted the Saturn's capability to take on passengers and cargo without ramps or stairs, making it suitable for small-town airports with limited facilities.[2]

Tony LeVier piloted the first flight on June 17, 1946. Lockheed had received 500 conditional orders for this aircraft, priced at $85,000 each. But, by the time the design was completed, the selling price had risen to $100,000 and these orders had been cancelled, with war surplus C-47s filling the same market at a quarter the price. Lockheed lost $6 million from the development of the two prototypes, which were scrapped in 1948.

Specifications

[edit]

Data from Francillon, p. 281

General characteristics

  • Crew: Two
  • Capacity: 14 passengers
  • Length: 56 ft 6 in (15.69 m)
  • Wingspan: 74 ft 0 in (22.56 m)
  • Height: 19 ft 10 in (6.05 m)
  • Wing area: 502 sq ft (46.6 m2)
  • Empty weight: 11,361 lb (5,153 kg)
  • Gross weight: 16,000 lb (7,257 kg)
  • Powerplant: 2 × Wright 744C-7BA-1 seven cylinder radial engine, 700 hp (522 kW) each

Performance

  • Maximum speed: 198 kn (228 mph, 367 km/h) at sea level
  • Cruise speed: 163 kn (187 mph, 301 km/h)
  • Range: 522 nmi (600 mi, 965 km)
  • Service ceiling: 26,500 ft (8,075 m)
  • Rate of climb: 1,325 ft/min (6.7 m/s)

References

[edit]
Notes
  1. United Press, “Lockheed Will Build Short-Haul Transport”, The San Bernardino Daily Sun, San Bernardino, California, Monday 20 November 1944, Volume 51, page 1.
  2. "Pinup - Lockheed Saturn", January 1946, Popular Science bottom of page 96 with good photo on following page
Bibliography
  • Boyne, Walter J., Beyond the Horizons: The Lockheed Story. St. Martin's Press: New York, 1998.
  • Francillon, René J. Lockheed Aircraft since 1913. London:Putnam, 1982. ISBN 0-370-30329-6