Skip to content
Welcome To Our Store.
100,000+ Products for Home, Medical, Office & Classroom Needs
Search
Skip to product information
1 of 1

Apollo Guidance, Navigation and Control: Design Survey of the Apollo Inertial Subsytem - Paperback

$33.68 USD
$33.68 USD
Sale Sold out
Shipping calculated at checkout.
In stock (100 units), ready to be shipped

Available Offers

Fastest Delivery Tomorrow With Vip DealOrder within 1 hr 8 mins.

Instant 10% Discount On HDFC Banks Credit/Debit Cards EMI and CreditCard

Secure checkout with
  • American Express
  • Apple Pay
  • Diners Club
  • Discover
  • Google Pay
  • Mastercard
  • PayPal
  • Shop Pay
  • Visa

Flight Range: Up to 1,000 meters (3,280 feet)

Maximum Speed: 45 kilometers per hour (28 miles per hour)

For all orders exceeding a value of 100USD shipping is offered for free.

Returns will be accepted for up to 10 days of Customer’s receipt or tracking number on unworn items. You, as a Customer, are obliged to inform us via email before you return the item.

Otherwise, standard shipping charges apply. Check out our delivery Terms & Conditions for more details.

View Product Details
Shopping cart
Product Product subtotal Quantity Price Product subtotal
Apollo Guidance, Navigation and Control: Design Survey of the Apollo Inertial Subsytem - Paperback
Apollo Guidance, Navigation and Control: Design Survey of the Apollo Inertial Subsytem - Paperback
Apollo Guidance, Navigation and Control: Design Survey of the Apollo Inertial Subsytem - Paperback
$33.68/ea
$0.00
$33.68/ea $0.00

Product Description

by Mit (Author), Nasa Manned Spacecraft Center (Author), William a. Stameris (Editor)

The Design Survey of the Apollo Inertial Subsystem was funded by NASA under Contract NAS-l2-642. This contract was administered by the NASA Electronics Research Center of Cambridge, Massachusetts. The purpose of this document is to record the history of the Apollo Inertial Subsystem design and development (CSM and LM) in order to provide a source document for subsequent design criteria monographs. The record provided by this document covers the de sign, development, and testing of an inertial subsystflm intended for manned spaceflight beyond earth orbits. In addition, it highlights the experience and knowledge accumulated by this portion of the Apollo program. Finally, technical and program-oriented recommendations have evolved naturally from the experience documented and such recommendations are given as an important part of this Design Survey.

Number of Pages: 194
Dimensions: 0.41 x 9.69 x 7.44 IN
Illustrated: Yes
Publication Date: June 19, 2012
you might like